Enclosure 2 - Description of GFE Aircrafts
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Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
1(195)
Enclosure 2 – Description of GFE Aircrafts
1 GFE Aircraft Learjet LR35A ..........................................................................................4
1.1 Learjet LR35A Aircraft Maintenance Program ........................................................4
1.1.1 Comprehensive description of Learjet Maintenance Program (MM-99) ...............4
1.1.2 Modifications that affects the maintenance program ............................................5
1.1.3 Airframe Maintenance Documentation ................................................................5
1.1.4 Engine Maintenance Documentation ...................................................................5
1.1.5 Maintenance Tasks related to changes .................................................................6
1.1.6 Guiding documents issued by the Agency and Aviation Authority for both
Airframe and Engines: ....................................................................................................6
1.2 GFE Aircraft Learjet 35A SE-DHO.........................................................................7
1.2.1 Aircraft Specification ..........................................................................................7
1.2.2 Engines ...............................................................................................................7
1.2.3 Avionics ..............................................................................................................7
1.2.4 Mission System ...................................................................................................8
1.2.5 Mission Cable Harness to Hard Points .................................................................9
1.2.6 Antenna layout .................................................................................................. 10
1.2.7 Inspection due times and dates .......................................................................... 11
1.2.8 Implemented Changes ....................................................................................... 12
1.3 GFE Aircraft Learjet 35A SE-DHP ....................................................................... 28
1.3.1 Aircraft Specification ........................................................................................ 28
1.3.2 Engines ............................................................................................................. 28
1.3.3 Avionics ............................................................................................................ 28
1.3.4 Mission System ................................................................................................. 29
1.3.5 Mission Cable Harness to Hard Points ............................................................... 30
1.3.6 Antenna layout .................................................................................................. 30
1.3.7 Inspektion due times and dates .......................................................................... 31
1.3.8 Implemented Changes ....................................................................................... 32
2 GFE Aircraft Mitsubishi MU-2 ..................................................................................... 47
2.1 Mitsubishi MU-2 Aircraft Maintenance Program .................................................. 47
2.1.1 Comprehensive description of Mitsubishi Maintenance Requirements Manual
(MR-0178-2): ............................................................................................................... 47
2.1.2 Modifications that affects the maintenance program .......................................... 47
2.1.3 Maintenance Documentation ............................................................................. 48
2.1.4 Guiding documents to be used during maintenance: .......................................... 48
2.1.5 Maintenance Tasks related to changes ............................................................... 48
2.1.6 Guiding documents issued by the Agency and Aviation Authority for both
Airframe and Engines: .................................................................................................. 49
2.2 GFE Aircraft Mitsubishi MU-2 SE-GHA .............................................................. 50
2.2.1 Aircraft Specification ........................................................................................ 50
2.2.2 Engines ............................................................................................................. 50
2.2.3 Propeller ........................................................................................................... 50
2.2.4 Avionics ............................................................................................................ 50
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2.2.5 Mission System ................................................................................................. 51
2.2.6 Mission Cable Harness to Hard Points ............................................................... 51
2.2.7 Antenna Layout ................................................................................................. 52
2.2.8 Inspection due times and dates .......................................................................... 53
2.2.9 Implemented Changes ....................................................................................... 54
2.3 GFE Aircraft Mitsubishi MU-2 SE-GHB .............................................................. 75
2.3.1 Aircraft Specification ........................................................................................ 75
2.3.2 Engines ............................................................................................................. 75
2.3.3 Propeller ........................................................................................................... 75
2.3.4 Avionics ............................................................................................................ 75
2.3.5 Mission System ................................................................................................. 76
2.3.6 Mission Cable Harness to Hard Points ............................................................... 76
2.3.7 Antenna Layout ................................................................................................. 77
2.3.8 Inspection due times and dates .......................................................................... 78
2.3.9 Implemented Changes ....................................................................................... 79
2.4 GFE Aircraft Mitsubishi MU-2 SE-GHD .............................................................. 99
2.4.1 Aircraft Specification ........................................................................................ 99
2.4.2 Engines ............................................................................................................. 99
2.4.3 Propeller ........................................................................................................... 99
2.4.4 Avionics ............................................................................................................ 99
2.4.5 Mission System ............................................................................................... 100
2.4.6 Mission Cable Harness to Hard Points ............................................................. 100
2.4.7 Antenna Layout ............................................................................................... 101
2.4.8 Inspection due times and dates ........................................................................ 102
2.4.9 Implemented Changes ..................................................................................... 103
2.5 GFE Aircraft Mitsubishi MU-2 SE-GHF ............................................................. 123
2.5.1 Aircraft Specification ...................................................................................... 123
2.5.2 Engines ........................................................................................................... 123
2.5.3 Propeller ......................................................................................................... 123
2.5.4 Avionics .......................................................................................................... 123
2.5.5 Mission System ............................................................................................... 124
2.5.6 Mission Cable Harness to Hard Points ............................................................. 124
2.5.7 Antenna Layout ............................................................................................... 125
2.5.8 Inspection due times and dates ........................................................................ 126
2.5.9 Implemented Changes ..................................................................................... 127
2.6 GFE Aircraft Mitsubishi MU-2 SE-IOV .............................................................. 147
2.6.1 Aircraft Specification ...................................................................................... 147
2.6.2 Engines ........................................................................................................... 147
2.6.3 Propeller ......................................................................................................... 147
2.6.4 Avionics .......................................................................................................... 147
2.6.5 Mission System ............................................................................................... 148
2.6.6 Mission Cable Harness to Hard Points ............................................................. 148
2.6.7 Antenna Layout ............................................................................................... 149
2.6.8 Inspection due times and dates ........................................................................ 150
2.6.9 Implemented Changes ..................................................................................... 151
2.7 GFE Aircraft Mitsubishi MU-2 SE-IUA .............................................................. 171
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2.7.1 Aircraft Specification ...................................................................................... 171
2.7.2 Engines ........................................................................................................... 171
2.7.3 Propeller ......................................................................................................... 171
2.7.4 Avionics .......................................................................................................... 171
2.7.5 Mission System ............................................................................................... 172
2.7.6 Mission Cable Harness to Hard Points ............................................................. 172
2.7.7 Antenna Layout ............................................................................................... 173
2.7.8 Inspection due times and dates ........................................................................ 174
2.7.9 Implemented Changes ..................................................................................... 175
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1 GFE Aircraft Learjet LR35A
1.1 Learjet LR35A Aircraft Maintenance Program
1.1.1 Comprehensive description of Learjet Maintenance Program (MM-99) The maintenance is (according to Learjet Maintenance Manual MM-99) based on 24 Phase
Inspections, accomplished one at a time, in groups or collectively, as scheduled by the aircraft
operator and in accordance with allowable inspection tolerances.
Estimated utilization is 500 Hrs per A/C and year.
Each Phase Inspection is contained within one of four (1 of 4) hourly or calendar driven
inspection intervals, the 300 hour or 12 month A-Phases, 600 hour or 24 month B-Phases,
1200 hour or 48 month C-Phases and 2400 hour or 96 month D-Phases.
Each of the primary inspection intervals (A, B, C, and D) contains six (6) stand-alone Phase
Inspections.
Inspection list according to Learjet maintenance Manual MM-99:
• Phase A2 300 hrs Inspection / Checks.
• Phase A3 300 hrs Inspection / Checks.
• Phase A4 300 hrs Inspection / Checks.
• Phase A5 300 hrs Inspection / Checks.
• Phase A6 300 hrs Inspection / Checks
• Phase B1 600 hrs Inspection / Checks
• Phase B2 600 hrs Inspection / Checks.
• Phase B3 600 hrs Inspection / Checks
• Phase B4 600 hrs Inspection / Checks.
• Phase B5 600 hrs Inspection / Checks.
• Phase B6 600 hrs Inspection / Checks.
• Phase C1 1200 hrs Inspection / Checks.
• Phase C2 1200 hrs Inspection / Checks
• Phase C3 1200 hrs Inspection / Checks
• Phase C4 1200 hrs Inspection / Checks.
• Phase C5 1200 hrs Inspection / Checks
• Phase C6 1200 hrs Inspection / Checks.
• Phase D1 2400 hrs Inspection / Checks.
• Phase D2 2400 hrs Inspection / Checks
• Phase D3 2400 hrs Inspection / Checks
• Phase D4 2400 hrs Inspection / Checks
• Phase D5 2400 hrs Inspection / Checks.
• Phase D6 2400 hrs Inspection / Checks.
• 3000 Landings Inspections.
• Major Landing Inspections.
• 12 Year Airframe Inspections
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• 12000 Hours Airframe Inspections.
• Other Interval Inspections.
• Unscheduled Maintenance Checks.
• MPI Engine Zone Inspection.
• Engine Light Maintenance TFE731-2.
1.1.2 Modifications that affects the maintenance program
• The wings have been modified with hard points to carry ECM pods and outboard
winches.
• The R/H wing tip tank has been modified with tip radome covering antennas for an
inboard ECM system ASTOR.
• To supply the ECM equipment with 3-phase AC, one 3kVA inverter system has been
installed in the inboard aft baggage area. (FAA STC SA125NE).
• Operator Stand is installed in the cabin with equipment to control winches and ECM
units. Set of monitoring equipment as TV-camera, mirrors etc.
• Aft Body Strakes in accordance with AVCON STC ST00432WI (EASA/LBA
TA0112) have been installed.
• Alteration between Dual / Single Mid Fuselage Camera Pods and Structural Plugs in
accordance with AVCON STC SA2479CE (EASA.IM.A.S.01449).
1.1.3 Airframe Maintenance Documentation Maintenance of the airframe is conducted according to the following documentation:
• Learjet Maintenance Manual. MM-99
• Learjet Wiring Manual. WM-99
• Learjet Illustrated Parts Catalogue.
• Learjet Service Bulletins.
• Learjet Airplane Accessory Kit.
• Learjet Airplane Modification Kit.
• Learjet Structural Repair Manual.
• Learjet Non-Destructive Inspection Manual.
• Keith TR-134 System Service Manual. TR-134.
• Saab AB, Technical Directives-Modification, issued by DOA EASA 21J.108.
Continued Airworthiness.
1.1.4 Engine Maintenance Documentation Maintenance of the engines is conducted according to the following documentation:
• Honeywell TFE731 Light Maintenance Manual. 72-02-01
• Honeywell TFE731 Illustrated Pars Catalogue. 72-00-71.
• Honeywell TFE731 Service Bulletin for Service Life Limits of Critical Life Limited
Components. SB TFE731-72-3001.
• Honeywell TFE731 Service Bulletins.
• Honeywell TFE731 Service Information Letters.
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1.1.5 Maintenance Tasks related to changes The following maintenance tasks are not included in the aircraft manufactures’ maintenance
manual. The tasks are included in the operators AMP:
• Structural Plugs in Cabin Annual/300 hrs Inspection/Checks
• Operator’s Consol. Annual/300 hrs Inspection/Checks
• Mission Power Annual/300 hrs Inspection/Checks
• Mission Power 600 hrs Inspection/Checks
• Mission Power 1200 hrs Inspection/Checks
• ACAS II. 24 Months Inspection/Checks
• Special Operational Fatigue Inspection 1200 hrs Inspection/Checks
• Hard Points and ejection unit 300 Hrs Inspection
1.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines:
• FAA Airworthiness Directives.
• Swedish NAA LVD.
• EASA AD.
• EC 2042/2003 Annex II Part-145- AMC. & Guidance Material.
• BCL - C, -D, -M if operating under Swedish regulations
• EASA Series-OPS
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1.2 GFE Aircraft Learjet 35A SE-DHO
1.2.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
Learjet
35A
195 SE-DHO 13320 8780 2012-11-23
1.2.2 Engines Type: TFE731-2-2B
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours
remaining to
MPI:
Hours
remaining to
CZI:
Left Engine P-74278 11122 7392 928 922
Right Engine P-74583 10648 7406 179 170
1.2.3 Avionics System: Type / Part Number: Note:
Autopilot JET FC 200
Dual VHF-COM Collins VHF-22C
HF-COM Collins 718U-5
ICS & Audio System DB System
Dual VHF-NAV Collins VIR-30A
GPS Garmin GPS 165 TSO
Dual DME Collins DME40
ADF 1 Bendix/King KDF-805
XPDR 1 & 2 Collins TDR94D Mode S
EHS
TCAS II Collins TCAS-4000
Dual TCAS II VSI/RA/TA Indicator Collins TVI-920
TAWS / EGPWS Honeywell MK VIII
RDR ALT Collins ALT-55B
Weather Radar Honeywell Primus 400
MFD Display Honeywell MFRD
ELT Kanad ELT 406-AF-H
Dual Mach Airspeed indicator IDC 2680003-2
Altimeter incl. encoder LH IDC 518-16007-187
Altimeter RH IDC 23932-053
Altitude Report & Alerting System IDC 23989-011
Air Data Display Unit 9D-80130-32
Dual Flight Director Indicator Collins 329B-7R-2
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Dual VG-Gyro JET VG-206(XX)
Standby Altitude Gyro JET AI 804
Dual Horizontal Situation Indicator Collins 331A-6R
Dual RMI Collins 332C-10
Dual DG-Gyro JET DN-101D
RVSM
FDR Sundstrand 980-4100-FWUS
CVR Fairchild 93-A100-83
1.2.4 Mission System System: Description:
Fixed general installations
FR31 VHF/UHF COM Radio
AN/ARC 182 VHF/UHF COM Radio
GPS MAP System
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
KGS SPS-3052B Inverter 230VAC 50Hz
Laser Prism
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ASTOR Fixed installed system
ADRIAN C & S Pod mounted system
U95-N Pod mounted system
U95-D2 Pod mounted system
U95 Sorc Pod mounted system
A100 Pod mounted system
Missile Threat Simulator
DARTS Pod mounted system
GMS Pod mounted system
Chaff Dispenser
BOX 3 Pod mounted system
Target Towing
MTR 101 Outboard pod mounted winch
AS200 MDI (Miss Distance Indicator)
TLX Height keeping target
Precisions GPS Pos System
TAPS
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1.2.5 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, U95-N,
U95-D2, U95 Sorc,
A100, DARTS, GMS,
BOX 3 and MTR 101
General Signal Harness General Signal Harness Two pair shielded
AWG 20 x 25
MTR 101 MTR 101 Harness MTR 101 Harness Two pair shielded
AWG 20 x 3
AWG 16 x 4 +
shield
U95-N, U95-D2, U95
Sorc, A100 and GMS
MIL-STD-1553B Data
Bus
MIL-STD-1553B Data
Bus
Twinax x 8
U95-N, U95-D2, U95
Sorc, A100, DARTS,
GMS and BOX 3
AC Power
115/200VAC 400 Hz 3-
Phase 3 x 10 A
AC Power 115/200VAC
400 Hz 3-Phase 3 x 10 A
AWG 12 x 10 +
shield
Adrian C & S, GMS
and BOX 3
DC Power 28 VDC 150
A
DC Power 28 VDC 150
A
AWG 4 x 4
MTR 101 Coaxial 2 x 75 Ω Coaxial 2 x 75 Ω
Adrian C & S Coaxial 3 x 50 Ω Coaxial 3 x 50 Ω
Recognition Light Recognition Light
Cable
Recognition Light Cable AWG 16 x 4 +
shield
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1.2.6 Antenna layout
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1.2.7 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Due Landings
Aircraft SE-DHO
Phase A 300 hour insp. AMP 2012-07-16 13290 13590,3 2013-09-10
Phase B 600 hour insp. AMP 2011-03-05 13043 13643,3 2013-04-05
Phase C 1200 hour insp. AMP 2009-11-01 12849 14049,1 2013-10-31
Phase D 2400 hour insp. AMP 2009-08-18 12789 15189,6 2017-08-16
Special operational fatigue inspect AMP 2009-01-23 12620 13820,8
12000 Hrs Inspection AMP 2001-08-29 11269 17269,1
45 days insp. AMP 2012-10-19 13303 2012-12-03
6 Month Inspection AMP 2012-07-17 13290 2013-03-11
2 Year Inspection AMP 2011-06-17 13129 2013-07-20
12 Year Airframe inspection AMP 2001-08-28 2013-08-25 13503
MPI engine zone inspecition LH AMP 2009-10-22 12849 14249,1
MPI engine zone inspecition RH AMP 2005-04-12 12053 13453,6
300 Hrs Inspection AMP 2011-10-11 13182 13500
1200 Hrs Inspection AMP 2007-05-15 12440 13640
3000 Landing Inspection AMP 1996-01-24 9000
6000 Major Landing Gear Inspection AMP 1988-10-11 10745
Operator's Console 300h/1y insp. AMP 2012-04-23 13248 13548,8 2013-04-23
ACAS 2 (TCAS) 24month insp. AMP 2011-06-29 13129 2013-07-13
Mission equipment 300 hour insp. AMP 2012-07-19 13290 13590,3
Engine S/N P-74278 Remaining
Engine 150 hrs insp. AMP 13431,82 111,34
Engine 300 hrs insp. AMP 13449,1 128,62
Engine 800 hrs insp. AMP 13649,1 328,62
Engine Compressor Zone Insp. AMP 14243,3 922,82
Engine Major Periodic Inspection AMP 14249,1 928,62
Engine S/N P-74583 Remaining
Engine 150 hrs insp. AMP 13440,3 119,82
Engine 300 hrs insp. AMP 13471,8 151,32
Engine 800 hrs insp. AMP 13696 375,52
Engine Compressor Zone Insp. AMP 13490,8 170,32
Engine Major Periodic Inspection AMP 13499,9 179,42
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1.2.8 Implemented Changes
Abbreviations:
Abbr. Issued by Explanation
AAK Learjet Aircraft Accessory Kit
AD EASA, FAA Airwortness Directive
AMK Learjet Aircraft Mod Kit
AW Learjet Accessory Wire
LVA LFV Luftvärdighetsanvisning
LVD LFV Luftvärdighetsdirektiv
SB Keith, Learjet, Nyge Service Bullentin
SIL Rockwell Service information letter
SSB Nyge and Garmin Sofware SB
SSK Learjet Special Spares Kit
STC Avcon, Flight Int., Keith,
EASA
Supplement Type Certificate
TDM Nyge Tekniskt Direktiv Materiel
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Status date November 23rd
2012.
SB/AD etc Reference
Rev Subject Document reference Eff. date Rev Compliance Status Remarks
AVCON, Avcon Industries, Inc.
AVCON STC SA00432WI
R Install. Avcon Fins 31-Mar-2005 R 01-Jul-2005
AVCON STC SA2479CE
A Install. Plug of Dual Hatches 30-Jun-2005 A 01-Jul-2005
AVCON STC ST00564WI
AFM suppl. increase T/O weight........ 25-Aug-1997 29-Jun-2005
AVCON STC ST00611WI
C Increase Takeoff Weight to 19600 pounds
11-Mar-2005 C 01-Jul-2005
AVCON STC ST00612WI
B Increase Wing/Tip Zero Fuel Weight 28-Nov-1997 B 01-Jul-2005
AVCON STC ST00613WI
C Increase Landing Weight to 16000 pounds
11-Mar-2005 C 01-Jul-2005
EASA, European Aviation Safety Agency
EASA AD 2006-0265
Incorrect transponder altitude 30-Aug-2006 18-Aug-2009
EASA AD 2008-0159
Improve EHS Operation HONEYWELL SB MST 67A-34-56 HONEYWELL SSBMST 67A-SW5 Rev 1
25-Aug-2008 01-Dec-2010 N/A N/A by transponder P/N installed
EASA AD 2009-0097
IR Mode S Transponder -Check/Modification
DHC SB 8-34-243 Rev A EASA AD 2010-0067 ROCKWELL SIL07-1
29-Apr-2009 IR 18-Aug-2009 PCW Are in compliance with EASA AD2009-0097 Ref TDM03-17 DWG MF1030064-1 Rev.C
EASA AD 2009-0173
1 Mode S Transponder Mod/Repl 30-Sep-2010 1 08-Dec-2010 N/A due to ADC p/n
EASA AD 2009-0251-E
Portable Fire Extinguishers-Ident/Repl
25-Nov-2009 07-May-2010 N/A N/A by current P/N installed
EASA AD 2009-0262
Halon 1211 Fire Extinguishers Id/Repl
EASA AD 2009-0278 FFE ASB26-115 Rev C
15-Dec-2009 07-May-2010 N/A N/A by current P/N installed
EASA AD 2009-0278
Halon 1211 Fire Extinguishers Id/Repl
EASA AD 2009-0262 22-Dec-2009 07-May-2010 N/A N/A by current P/N installed
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EASA AD 2010-0003
R1 Mode S Transponder -Check/Modification
11-Jan-2010 R1 10-Mar-2010 N/A due to p/n
EASA AD 2010-0204
IR Mode S Transponder -Mod/Repl 06-Oct-2010 IR 08-Dec-2010 N/A by ADC p/n installed
EASA AD 2012-0037
KIDDE GRAVINER HAND OPERATTED FIRE EXTINGUISHER
10-Sep-2012
FAA, U.S, Federal Aviation Administration
FAA, U.S AD 2000-24-19
Donning oxygen masks 22-Nov-2000 20-Feb-2003 Complied with by insert of AFM Change 12
FAA, U.S AD 2001-07-11
Goodyear Flight Eagle Tire Tread Separat
LEARJET AW 32-021 01-May-2001 17-May-2001 N/A by s/n on tire
FAA, U.S AD 2001-15-17
Prevent erroneous altitude interpretatio
20-Aug-2001 12-Feb-2009 N/A due to p/n
FAA, U.S AD 2004-03-08
To prev. structural damage to eng.pylons
LEARJET SB 51-03 LEARJET SB 51-04 Rev 5
08-Mar-2004 09-Mar-2004 SB 51-04 previous carried out.
FAA, U.S AD 2005-13-36
Detailed inspection of aileron cable. 09-Aug-2005 01-Nov-2005
FAA, U.S AD 2005-16-09
Inspection of Tip Tank Flapper Valves Supersedes AD 95-25-03
LEARJET SB 28-10 13-Sep-2005 14-Sep-2005 Flapper p/n 2323006-802 previously installed. No further action req.
FAA, U.S AD 2007-04-18
Modify Standby Fuel Pump switches LEARJET SB 28-11 Rev 5
23-Mar-2007 15-Mar-2007 Previusly complied with. Ref. Learjet SB 28-11
FAA, U.S AD 2007-17-17
Unsealed gaps in engine firewall 02-Oct-2007 11-Sep-2007 Previously carried out, ref. SB 54-03
FAA, U.S AD 2008-02-19
HP-Turbine Disc replacement. 19-Feb-2008 06-Feb-2008 N/A due to engine model.
FAA, U.S AD 2008-19-12
Remove from service ITT Duct 08-Aug-2012
FAA US AD 74-08-09
3 Transport category airplanes equipped with lavatories
11-May-2012
FAA, U.S AD 78-16-03
To precl. a fail. of the Refr. Cond. Fan Issued 1978-08-17
LEARJET SB 21-03 11-Dec-2000 20-Jan-1984
FAA, U.S AD 79-08-01
1 Aeronca thrust Reversers Suppl to AFM
19-Apr-1982 1 13-Feb-2009 N/A Aeronca Thrust Reversers not installed
FAA, U.S AD 80-06-02
Starter assisted airstart 24-Mar-1980 03-Dec-1993
FAA, U.S AD 80-07-09
Cabin Main Entrance Upper Door LEARJET AMK79-09 01-May-1980 25-Jun-1980
FAA, U.S AD 80-17-11
Airspeed Limitation Placard LEARJET SB 11-03 Rev A
28-Aug-1980 19-Aug-1987
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FAA, U.S AD 80-18-08
To Prevent loss of Emergency electrical Power............
28-Aug-1980 01-Jan-2003 N/A N/A due to Component p/n
FAA, U.S AD 80-19-09
1 Motive Flow Valve LEARJET AMK80-07 11-Dec-1980 1 05-Nov-1980
FAA, U.S AD 80-19-11
1 AFM insert LFV LVD1635 Rev A 20-May-1985 1 09-Feb-2006 Checked. Previously complied with.
FAA, U.S AD 81-04-06
Cockpit Voice Recorder A100 series 01-Apr-1981 12-Feb-2009 N/A due to model & s/n
FAA, U.S AD 81-13-07
To ensure oper. without fuel starvation
LFV LVA1748 25-Jun-1981 10-Aug-1981
FAA, U.S AD 82-01-05
2 Stall Warning Accelerometer Check LEARJET SB 27-12 Rev B LFV LVA1912
10-Apr-1986 2 30-May-2007 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24
FAA, U.S AD 83-08-03
Insp.RH Engine Hydraulic Pressure Line for Interference.
LEARJET SB 29-01 Rev 1
03-May-1983 12-Apr-1983
FAA, U.S AD 84-19-06
To prevent Aileron/Trim Tab Flutter due to failure of the trim tab ctrl system
22-Oct-1984 01-Oct-2009 PCW
FAA, U.S AD 84-20-06
Inspect LH Hydraulic Lines for Interfere superseded by 86-22-05
LEARJET SB 29-02 20-Feb-1987
FAA, U.S AD 85-16-04
Airplane Lateral Control Characteristics
FAA, U.S AD 96-19-13 LEARJET AMK83-05 LFV LVD2034
06-Sep-1985 06-Feb-2002 N/A due to config. (STC SA766NW never been installed).
FAA, U.S AD 85-22-10
Collins HSI & FD indicators 31-Dec-1985 15-Jun-2009 N/A by p/n & s/n
FAA, U.S AD 86-05-05
1 Relocation of Battery Vent Inlet Fitting
LEARJET SB 24-10 LFV LVD2046
19-Jan-1988 1 10-Dec-1985
FAA, U.S AD 86-22-05
To prevent of flap operation.......... LEARJET AMK86-04 10-Nov-1986 20-Feb-1987
FAA, U.S AD 87-02-06
Insp. of Fwd. Eng.Mounts for Cracks LEARJET SB 71-03 Rev 1
06-Feb-1987 17-Jan-2005 Para.A: see Phase A3 300 hour insp. Para.B: see A/C status RAL
FAA, U.S AD 87-04-06
Autopilot FC-530 Limitations 09-Mar-1987 12-Feb-2009 N/A due to A/P model
FAA, U.S AD 87-06-09
Inspection of Mechanical Prod. C/B's 27-Apr-1987 01-Oct-2009 PCW Ref. Jet East Inc. 25 july 1988 (gammal aircraft logbook)
FAA, U.S AD 89-12-01
Inspection of Drag Chute Riser LEARJET SB 25-07 Rev A
03-Jul-1989 01-Oct-2009
FAA, U.S AD 90-09-10
Replace Texas Instr. Circuit Breakers 30-May-1990 01-Oct-2009 N/A due to type of C/B not installed in aircraft Ref. Learjet PC.
FAA, U.S AD 91-03-08
Deactivation of Forward Cabinet and Overhead Fluoriscent Light Circuits
LEARJET SB 33-05 Rev A
12-Feb-1991 22-Sep-2009 Post mod SB 33-06A
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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16(195)
FAA, U.S AD 92-19-12
SYSTEM TUBE (W-IN 30D) LEARJET AMK90-05 17-Nov-1992 17-Jun-1993
FAA, U.S AD 94-21-06
Safety belt LFV LVD2588 25-Nov-1994 01-Oct-2009 N/A due to p/n
FAA, U.S AD 95-19-04
1 Omega Navigation System 27-Mar-2000 1 03-Dec-2010 AD note cancelled
FAA, U.S AD 95-20-03
Insp.of Cabin Pressurization Outflow....
LEARJET SB 21-19 02-Nov-1995 24-Jan-1996
FAA, U.S AD 95-22-01
IR ALC Series 66 fluorescent lamps 07-Aug-2012
FAA, U.S AD 95-25-03
Inspection of Tip Tank Flapper Valves
LEARJET SB 28-10 27-Dec-1995 24-Jan-1996
FAA, U.S AD 96-19-13
Raisbeck Group STC SA766NW FAA, U.S AD 85-16-04 LEARJET AMK83-05
22-Oct-1996 09-Feb-2006 N/A due to config. (STC SA766NW never been installed).
FAA US AD 97-05-03
1 GNS XLS and GNS XL system 01-Nov-2011
FAA, U.S AD 98-06-28
Electrical Arcing and Fire Hazard LEARJET SB 21-24 Rev 1
24-Apr-1998 15-Sep-2009 N/A due to s/n
FAA, U.S AD 98-25-10
1 Inspection of seat restraint system LFV LVD2929 Rev 2 14-Jan-2000 1 01-Oct-2009 N/A due to manufacturing year
FAA, U.S AD 99-08-21
Oxygens Masks 02-Jun-1999 30-Sep-2009 N/A due to different cure date
FAA, U.S AD 99-23-19
Replacement or Spoiler Actuator LEARJET SB 27-36 28-Oct-1999 12-Feb-2009 N/A due to s/n
FLIGHT INT, Flight international inc.
FLIGHT INT STC SA1604SO
Hard points 26-nov-99 17-nov-88
KEITH, Keith Products, Inc.
KEITH SB 163 B Load Shed Installation 19-Nov-1999 15-May-2007
KEITH SB 166 A Belt Guard Installation 08-Oct-2001 15-May-2007
KEITH STC ST09366SC
Install. of Electric-Driven Vapor A/C 12-Aug-1997 21-Jul-1999
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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17(195)
LEARJET, Bombardier, LEARJET
LEARJET AAK 76-03
WING ICE L. 30-Jun-1976 10-Nov-1988
LEARJET AAK 78-03
A MLG OLEO ST PISTON 30-Jun-1978 A 10-Dec-1985
LEARJET AAK 79-02
PITOT HEAT IND. 30-Jun-1979 25-Jul-1988
LEARJET AAK 79-04
CONICAL FAN SPINNER 30-Jun-1979 10-Nov-1988
LEARJET AAK 80-02
INCREASE T.O. WEIGHT 30-Jun-1980 10-Dec-1985
LEARJET AAK 80-03
INCREASE LAND.WEIGHT 30-Jun-1980 10-Dec-1985
LEARJET AAK 81-01
1 Starter Contactor 30-Jun-2008 1 16-Sep-2008 PCW
LEARJET AAK 82-02
1 Install. Cabin Temp.Contr.Syst.filters 01-Oct-1982 1 22-Jan-2003 Final complied w/o C04708
LEARJET AAK 85-08
GS ANTENNA 30-Jun-1985 10-Dec-1985
LEARJET AAK 86-02
1 Inst. of LDG Actuator Down Lock Switch
22-Sep-2008 1 04-Nov-2008 Checked PCW.
LEARJET AAK 89-03
Installation of Doublers at Frame 6. 08-Jan-1990 29-Aug-2001 Installation doubler at frame #6 on R/H side
LEARJET AAK 89-04
D Inst. of Doublers at Frame 7 11-Aug-1995 D 29-Aug-2001
LEARJET AAK 89-14
25 DG.FLAP LIMIT SWITCH 30-Jun-1989 02-May-1990
LEARJET AAK 90-12
1 Inst. of Batting at Wing Spar 1 Splice 22-Sep-2008 1 04-Nov-2008 Checked PCW.
LEARJET AAK 90-16
IR Overhead Fluorescent Light. Wiring Prov.
30-Jan-1991 IR 22-Sep-2009
LEARJET AAK 91-05
1 Inst of Defog Temperature Sensors 16-Feb-2009 1 05-Jun-2009 N/A Due to Electric Windshield not installed
LEARJET AMK 78-02
2 DOOR HANDLE 30-Jun-1978 06-Feb-1991 N/A due to s/n of aircraft.
LEARJET AMK 78-08
A GENERATOR DRIVE SPLINES DRIVE SHAFT
30-Jun-1978 A 25-Jun-1980
LEARJET AMK 78-12
A ENGINE BLEED AIR PLUMBING 30-Jun-1978 A 26-Jun-1979
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2012-12-06
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18(195)
LEARJET AMK 78-13
A ESS.BUS 04-Jun-2007 A 11-Sep-2007 Previously carried out, ref. AMK 78-13
LEARJET AMK 79-06
EMERG.PRES. VALVE 30-Jun-1979 22-Oct-1979
LEARJET AMK 79-07
GENERATOR DRIVE SPLINES 30-Jun-1979 25-Jun-1980
LEARJET AMK 79-09
CAB.DOOR MECHANISM (AD800709) (AD800709)
FAA, U.S AD 80-07-09 LFV LVA1613
30-Jun-1979 25-Jun-1980
LEARJET AMK 79-10
ENGINE FUEL TUBE 30-Jun-1979 25-Jun-1980
LEARJET AMK 80-06
A ENG.MOUNT (AD801711) (AD801711)
30-Jun-1980 A 27-Feb-1981
LEARJET AMK 80-07
MOTIVE FLOW VALVE (AD801909) (AD801909)
FAA, U.S AD 80-19-09 Rev 1 LFV LVA1625 Rev A
30-Jun-1980 05-Nov-1980
LEARJET AMK 80-17
1 Installation of Current Limiter Warning
28-Jun-2010 A 23-Jan-2009 Starter engage lamps, moved to opt. position
LEARJET AMK 81-17
HOR.STAB. HINGE PIN 30-Jun-1981 22-Jun-1982
LEARJET AMK 83-03
AILERON TRIM TAB BALANCE WEIGHT (AD84190 (AD84190
30-Jun-1983 01-Oct-2009 PCW
LEARJET AMK 83-05
WING STALL STRIP (AD851604) (AD851604)
FAA, U.S AD 85-16-04 FAA, U.S AD 96-19-13
30-Jun-1983 20-Feb-1987 N/A due to config. (STC SA766NW never been installed).
LEARJET AMK 85-01
A POWER DIST. 30-Jun-1985 A 24-Jan-1996
LEARJET AMK 86-04
WING FLAP SECTOR (AD862205) (AD862205)
FAA, U.S AD 86-22-05 30-Jun-1986 20-Feb-1987
LEARJET AMK 90-04
A Replacement of Parallelling Control Box
01-Aug-1992 26-Jan-1993
LEARJET AMK 90-05
SYSTEM TUBE (AD921912) (AD921912)
FAA, U.S AD 92-19-12 09-Oct-1991 05-Feb-1993
LEARJET AMK 91-2A
Windshield Anti-Ice Thermostat Replacem. Learjet SIL 30-005
12-Aug-1998 15-Nov-1999
LEARJET AW 32-021
Goodyear Flight Eagle Tire Tread Separat
FAA, U.S AD 2001-07-11 05-Feb-2001 17-May-2001 N/A by s/n on tire.
LEARJET SB 00-01
Inspection/Replacement of cables 27-Feb-2001 10-Apr-2001 Kontr.i status
LEARJET SB 05-01
FIRE EXT. BOTTLE (HYDROST.) 18-Nov-1992 21-Jun-1993
LEARJET SB 11-03
A AIRSPEED LIMIT PLACARDS AD841906
FAA, U.S AD 80-17-11 18-Sep-1980 A 19-Aug-1987
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2012-12-06
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19(195)
LEARJET SB 11-04
WASTE DISP.REC. PLACARDS AD740809
18-Dec-1981 23-Apr-1982 N/A due to model and s/n.
LEARJET SB 11-05
CREW SEAT BELT PLACARDS 31-Aug-1983 20-Oct-1980
LEARJET SB 11-06
BATTERY PLACARDS 21-Jul-1987 19-Aug-1987 N/A due to SB32-04 is carried out.
LEARJET SB 11-07
ID PLATE (O) 06-Nov-1992 01-Jan-1994
LEARJET SB 11-10
Repl.of Fuel Servicing Placards 17-Dec-2001 10-Dec-2003
LEARJET SB 21-03
CONDENSER FAN ASSY. AD781603
FAA, U.S AD 78-16-03 12-Jul-1978 20-Jan-1984
LEARJET SB 21-04
Inst. of Refrigeration Syst.Warn.Placard
22-Feb-1979 09-Feb-1979
LEARJET SB 21-05
CABIN PRES. SAFETY VALVE 18-Dec-1979 25-Feb-1980
LEARJET SB 21-06
Insp.of Air Distr.Sleeves & Clamps-Tailc
23-Sep-1980 27-Feb-1981
LEARJET SB 21-07
CABIN PRES. SAFETY VALVE (CHANGED) Garrett SB 5-2290
28-Oct-1980 12-Apr-1991
LEARJET SB 21-09
Insp.Cabin Press. Control Module for PN
12-Sep-1983 20-Jan-1984
LEARJET SB 21-12
Insp. of Pneumatic Duct Temp. Limiter
26-Sep-1989 10-Nov-1990
LEARJET SB 21-14
1 OUTFLOW VALVE SAFETY VALVE (R)
03-Jan-1995 1 24-Jan-1996 Superseded by SB 21-19.
LEARJET SB 21-15
2 Repl. of Refrig.Syst. Press Switch 22-Jul-2005 2 11-Oct-2005 N/A to Keith R34.
LEARJET SB 21-16
Mod. of Aux Cabin Heater Relay Assy
16-May-1994 13-Apr-2006
LEARJET SB 21-18
3 Imp.W-shield Aux.Defog & Aux.Crew Heat
11-Aug-2008 3 04-Nov-2008 N/A N/A due to AAK86-1 not incorporated
LEARJET SB 21-19
Insp.of Cabin Press.Outflow & Safety Vlv 130406-21-A4011 R2,102850-21-A4021 R2
FAA, U.S AD 95-20-03 03-Jan-1995 24-Jan-1996
LEARJET SB 21-20
Repl. Cabin Press. Outflow valve Assy
14-Jul-1995 16-Sep-1999
LEARJET SB 21-22
1 Inst.of Cabin Air Syst. Electr.Connector
15-Aug-2003 1 03-Nov-2003 N/A due to s/n of aircraft.
LEARJET SB 21-24
1 Repl.of Aux.Cabin Heater Wiring FAA, U.S AD 98-06-28 13-Aug-1996 1 15-Sep-2009 N/A due to s/n
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2012-12-06
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20(195)
LEARJET SB 21-25
3 Inst.of Improved Refrigeration Comp.Asse
12-Nov-2007 2 06-Feb-2008 N/A Due to Keith Aircondition System TR-134 Installed
LEARJET SB 21-26
5 Mod.of Auxiliary Cabin Heather 16-May-2007 5 05-Mar-2012
LEARJET SB 22-03
Repl.of Yaw Damper Servo Sector Bolts
02-Feb-1979 03-Feb-1979
LEARJET SB 22-04
C Mod. of Mach Trim Computer J.E.T SB 501-1132-9E, -10B, -11
25-Mar-1980 C 20-Feb-1980
LEARJET SB 22-05
Mod.of FC-530/-535 Autopilot Computer
05-Jan-1987 12-Apr-1991 N/A N/A due to A/P model
LEARJET SB 22-07
3 Inst.of Autopilot Accelerometer Monitor
11-Jun-2007 2 29-May-2007 N/A AAK 83-2 not complied with.
LEARJET SB 23-03
2 Increased FOD Protection-Installation of Antenna Protection.
09-Jul-2001 2 11-Jan-2006 Previous revision carried out.
LEARJET SB 24-06
Insp.of Battery Vents for Obstruction 29-Sep-1980 21-Oct-1980
LEARJET SB 24-07
Current Limiter Box Moisture Proofing 15-Jan-1981 12-Apr-1991
LEARJET SB 24-08
Insp.of No.4 Gauge Electrical Cables 11-May-1982 26-Jan-1983
LEARJET SB 24-09
Insp.Fuses for Proper Prot.Covering & PN
19-Apr-1983 22-Jul-1983
LEARJET SB 24-10
Reloc.of Battery Vent Inlet Fitting AD860505
FAA, U.S AD 86-05-05 Rev 1
18-jul-85 10-Dec-1985
LEARJET SB 24-11
Add.of Ret.for Gen.Warn.Ctrl Box.Connect
01-Nov-1990 12-Apr-1991
LEARJET SB 24-15
1 Inst.of Concorde Sealed Lead-Acid Batt.
24-Mar-2008 1 04-Sep-2008
LEARJET SB 25-03
Insp.of Drag Chute Mechanism Bolt 10-Nov-1980 15-Jan-1981
LEARJET SB 25-04
A Insp.of Drag Chute Mech.for Proper Clear
11-Nov-1981 A 23-Nov-1986
LEARJET SB 25-06
Insp.Drag Chute Canister Lid Latch Screw
19-Feb-1987 12-Feb-1987
LEARJET SB 25-07
A Insp.of Drag Chute Riser FAA, U.S AD 89-12-01 22-Mar-1989 A 01-Oct-2009
LEARJET SB 26-02
A Verif.& Ident.of Eng.Fire Ext.Bottl.Wire
30-Apr-1991 A 17-Jun-1991
LEARJET SB 26-04
1 Engine Fire Element Insp./repl. 11-Aug-2008 1 04-Nov-2008 N/A N/A by s/n on elements
LEARJET SB 27-03
A Repl.of Primary Control Syst.Stop Bolts
12-Sep-1975 A 19-Aug-1997 Checked. Previously complied with.
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2012-12-06
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21(195)
LEARJET SB 27-09
Insp.of Wing Flap Actuators 19-Dec-1978 20-May-1975
LEARJET SB 27-10
Rework of Pilot/Copil.Ctrl Wheel Trim ..
19-Apr-1979 17-Aug-1979
LEARJET SB 27-11
Insp.of Aileron for Drain Holes 06-Nov-1979 01-Mar-1980
LEARJET SB 27-12
B Stall Warn.Accelerometer Op.Check FAA, U.S AD 82-01-05 Rev 2 LFV LVA1912
25-Sep-1981 B 30-May-2007 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24
LEARJET SB 27-14
Insp.of Welds on Rudder Pedal Supp.Assy
08-Sep-1983 20-Jan-1984
LEARJET SB 27-16
Insp.Flap Attach.Fittings for Cracks 27-May-1986 05-Sep-1986
LEARJET SB 27-24
Insp.of Ail.& Rudder Ctrl Cable Assy 08-Nov-1993 01-Jan-1994
LEARJET SB 27-33
Removal of Sealant from Aileron Rib 27-May-1997 19-Aug-1997
LEARJET SB 27-35
4 Inst.of Secondary Locking Feature 15-Aug-2003 4 03-Nov-2003 Previous rev. carried out.
LEARJET SB 27-36
Replacement of Spolier Actuator FAA, U.S AD 99-23-19 14-Dec-1998 12-Feb-2009 N/A due to s/n
LEARJET SB 27-40
6 Insp/Inst. of Flap Structure Components
16-Aug-2010 6 10-Nov-2011 PCW Previous revision carried out
LEARJET SB 27-43
Recalibration rosemount 19-Jan-2005 17-Mar-2005 N/A due to STC ST00321WI-D not complied with.
LEARJET SB 27-45
1 Insp. Spoiler panels 02-Apr-2012
LEARJET SB 28-02 INAKTIV
Insp.of Tip Tank Elect.Conduit for Damag
20-Feb-1976 12-Apr-1991
LEARJET SB 28-05 INAKTIV
Op.check of Fuel Jettison Valves 14-Feb-1980 23-Apr-1980
LEARJET SB 28-06
Insp.of Rec.for Field Rep.of Mot.Flow Vl
21-Aug-1980 09-Dec-1980
LEARJET SB 28-08
Insp.of Motive Flow Vlv Shroud Cover 27-Aug-1990 02-Nov-1990
LEARJET SB 28-10
Inspection of Tip Tank Flapper Valves
FAA, U.S AD 2005-16-09 FAA, U.S AD 95-25-03
06-Oct-1995 14-Sep-2005 Flapper p/n 2323006-802 previously installed. No further action req.
LEARJET SB 28-11
5 Inst.of Standby Fuel Pump Annunciators
FAA, U.S AD 2007-04-18 28-Sep-2009 5 26-Feb-2010 Rev. 1-4 PCW. AFM cheched for Change 14
LEARJET SB 28-14
2 Repl.of Tip Tank Flapper Valves 09-May-2001 2 29-Aug-2001
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2012-12-06
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22(195)
LEARJET SB 28-17
1 Inst.of Fuel Panel Overlay Blank. Plate
14-Jan-2004 1 30-Aug-2007 Cover installed
LEARJET SB 28-18
Insp./Repl. of Fuel Filter Elements 24-Aug-2009 30-Oct-2009 N/A due to filter p/n
LEARJET SB 29-01
1 Insp.RH Eng.Hydr.Press.Line for Interfer
FAA, U.S AD 83-08-03 10-Sep-1996 1 01-Nov-2005 N/A due to installation of reducingvalve 3000-1500 psi
LEARJET SB 29-02
Insp.LH Eng.Hydr.Lines for Interference
FAA, U.S AD 84-20-06 15-Jun-1983 23-Aug-1983
LEARJET SB 29-03
Insp.Hydr.Tube Assy & Wiring for Interf.
14-Jan-1985 18-Apr-1985
LEARJET SB 29-05
Repl.of Hydr.Reservoir Sight Glass Assy
07-Oct-1992 01-Jan-1994
LEARJET SB 30-01
Windshield Anti-Ice Timer Op. Check 19-Jan-1983 28-Feb-1983
LEARJET SB 30-10
1 Repl. of Wing Anti-Ice Transverse Duct
12-Feb-1999 1 04-Aug-2000
LEARJET SB 30-11
3 Inst.of High Current Capacity Wire 05-May-2008 3 04-Sep-2008 PCW
LEARJET SB 31-01
Repl.of Oil Press.Annunciator Cap Assy
26-Oct-1992 01-Jan-1994
LEARJET SB 32-03
Insp.of LG Brake & Torque Link for Inter
25-Aug-1981 12-Apr-1991
LEARJET SB 32-04
Repl.of LG Hydraulic Selector Valve 23-Jan-1989 06-Nov-1990
LEARJET SB 32-07
1 Inst.of MLG Lower Torque Arms 10-Nov-1995 1 13-Jan-2004
LEARJET SB 32-18
Inst.of Main Landing Gear Wheel Screens
19-Jan-1999 15-Mar-1999 N/A. Affected Wheel Assy not installed.
LEARJET SB 32-20
Repl.of Landing Gear Shuttle Valve Bolt
09-Mar-2000 30-Jun-2000 Found N/A to Part Number.
LEARJET SB 32-21
Repl.of Brake Valve Adjustment Screw
01-May-2000 29-Aug-2001
LEARJET SB 32-23
1 Mod landing gear squat switch wiring 09-Apr-2007 1 29-May-2007 Previously carried out
LEARJET SB 32-26
Insp/Repl of the Nose Gear Wheel Assy
18-Jan-2010 10-May-2010 N/A by s/n
LEARJET SB 33-03
Insp.& Mod. of LH Fwd Cabinet Light Assy
24-Apr-1985 12-Apr-1991 N/A N/A due to interior config.
LEARJET SB 33-05
A Deactiv.of Fwd Cabinet & Overhead Light.
FAA, U.S AD 91-03-08 / AD901406
21-Dec-1990 A 12-Aug-1991
LEARJET SB 33-06
A Activ.of Fwd Cabinet & Overhead Fluore..
12-Apr-1991 A 22-Sep-2009
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2012-12-06
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23(195)
LEARJET SB 34-04
Insp.of Static Ports 11-Jun-1982 21-Oct-1982
LEARJET SB 35-04
Replacarding Oxygen Bottle Shutoff Valve
27-Feb-2004 20-Sep-2004 N/A N/A by p/n on oxygen regulator
LEARJET SB 36-02
A Insp.& Repl.of Eng.Bleed Air Flex Tube..
25-May-1978 A 12-Apr-1991 N/A N/A by s/n on aircraft
LEARJET SB 36-03
Repl Air Bottle & Weight-Balance Change
14-Dec-2009 11-Mar-2010 Due to weighing after installation of bottle p/n 6600194-6
LEARJET SB 51-01
Insp.Baggage Comp.Struct. for Corrosion AD 84-12-03
18-Jul-1985 10-Dec-1985
LEARJET SB 51-03
Insp.of Forward Engine Beam Shear Web.
FAA, U.S AD 2004-03-08 01-Feb-2001 06-Sep-2001 N/A N/A due to SB 51-04 performed.
LEARJET SB 51-04
5 Rep.of Forward Engine Beam Shear Web
FAA, U.S AD 2004-03-08 12-Oct-2009 5 11-Mar-2010 No rework required
LEARJET SB 51-4
3 20-Jan-2005 No rework req.
LEARJET SB 52-04
Mod.of Access Door Lock Assemblies
16-Apr-1979 12-Apr-1991 Found N/A. No locks installed.
LEARJET SB 52-05
Insp.of Cabin Int.Liner-Areas Of Emerg..
04-Nov-1980 12-Apr-1991
LEARJET SB 52-06
Mod.of Lwr Cabin Door Hook Mechanism
18-Dec-1992 01-Jan-1994
LEARJET SB 52-07
Repl.of Lwr Cabin Door Cable & Handle As
15-Sep-1993 06-Feb-1995
LEARJET SB 52-10
1 Repl.of Upper Cabin Door Torsion Bar Arm
03-Jun-1999 1 20-Sep-1999 N/A. 24 inch door not installed.
LEARJET SB 53-07
Inspect for Tailcone Drains 18-Dec-1992 01-Jan-1994
LEARJET SB 53-08
Inst.of Nutplates on Circ.Br.Panel Suppo
14-Feb-1994 06-Feb-1995
LEARJET SB 53-10
1 Repl.of LowerStinger & Ventral Fin Skin
17-Mar-2008 1 14-May-2008 N/A Due to Avcon Fins STC ST00432WI
LEARJET SB 53-11
3 Mod.of Tailcone Ballast Weight Installat
01-Jun-2009 3 28-Jan-2010 N/A Not incorporated.
LEARJET SB 53-13
Insp. Intern. baggage comp. floor splice
16-Jan-2006 08-Mar-2006 N/A Due to S/N
LEARJET SB 54-01
Insp.for Silicon Firesleeve-Start&Gen Ca
11-Jun-1982 06-Oct-1982
LEARJET SB 54-03
Insp/Firewall Sealing Modification 16-Mar-2001 02-Nov-2005 R/H side carried out
LEARJET SB 54-04
Insp/Repl.of Upper and Lower Pylon Skins
08-Aug-2001 22-Mar-2002 N/A by s/n on aircraft.
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2012-12-06
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24(195)
LEARJET SB 55-01
Insp.Horiz.Stab.Hinge Assy for Cracks
16-Aug-1991 16-Aug-1991 N/A No Thrust Reversers installed.
LEARJET SB 55-04
2 Inst.of Doublers on Horiz.Stabili.Skin 23-Feb-2009 2 10-Jun-2009 PCW
LEARJET SB 55-05
Imp.of Horiz.Stabilizer Actuator Access
16-Jan-1998 30-Sep-1998
LEARJET SB 55-06
Mod.of Navigation Light Wiring Conduit
30-Aug-2004 13-May-2005
LEARJET SB 71-02
Eng.Firewall Sealing at Feed-Thru Condui
13-May-1982 15-Jul-1982
LEARJET SB 76-01
B Insp.of Eng. I.T.T. Cable Connectors 07-Nov-1983 B 22-Jul-1983
LEARJET SB A27-42
Insp/Repl.of Aileron Ctrl Cables 23-Dec-2002 12-Dec-2002 Cables N/A by cal.time.
LEARJET SB A30-03
ALCOHOL ANTI-ICE SYSTEM (W-IN 10H)
18-Dec-1992 26-Jan-1993
LEARJET SB A32-15
1 Insp.of Landing Gear Actuator Pistons
21-Apr-1997 1 17-Apr-1998
LEARJET SSK 980
Evaporator Assy. 10-Feb-1989 20-Jul-1994
LEARJET SSK 981
Repl. of Spoiler Act. Support Bracket 19-Dec-1986 04-Aug-2000 Carried out on R/H side, kit 2692006-4.
LEARJET SSK 993
2 Repl. of Landing Gear Wheel Bearings
21-Jan-1991 2 14-Oct-1997 see w/o C00671 for 2 wheels
LFV, Luftfartsverket LFV
LVA 1613 Modifiering av övre kabindörr LEARJET AMK79-09 27-May-1980 25-Jun-1980
LFV LVA 1625 A Till,gg i flyghandbok. T,thetskontroll FAA, U.S AD 80-19-09 Rev 1 LEARJET AMK80-07
23-Jun-1980 A 05-Nov-1980
LFV LVA 1748 Revision av Flyghandbok. Br,nslem,ngd
FAA, U.S AD 81-13-07 24-Aug-1981 10-Aug-1981
LFV LVA 1912 Periodisk kontroll av Stallvarning. FAA, U.S AD 82-01-05 Rev 2 LEARJET SB 27-12 Rev B
10-Nov-1983 30-May-2007 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24
LFV LVD 1635 A Revision Flyghandbok/kontr. A/P & mod.
FAA, U.S AD 80-19-11 Rev 1
15-Jul-1985 A 28-Sep-2009 PCW Ref. FAA AD 80-19-11 R1
LFV LVD 2034 Reducering av MMO FAA, U.S AD 85-16-04 30-Aug-1985 06-Feb-2002 N/A due to config. (STC SA766NW never been installed).
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2012-12-06
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25(195)
LFV LVD 2046 Kontroll av batterihållare FAA, U.S AD 86-05-05 Rev 1
25-nov-85 10-Dec-1985
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9 23-May-1991 17-Jun-1991 checked OK.
LFV LVD 2588 Byte av säkerhetsbälten FAA AD 94-21-06
FAA, U.S AD 94-21-06 05-Jan-1995 01-Oct-2009 N/A due to p/n
LFV LVD 2853 Periodisk funktionskontroll av nödutgång
23-Mar-1998 13-Aug-2010
LFV LVD 2929 2 Kontroll av bältens låsfunktion AD 98-25-10
FAA, U.S AD 98-25-10 Rev 1
13-Jan-2000 2 01-Oct-2009 N/A due to manufacturing year
LFV LVD 3148 Modif. Transponder kontrollpanel 17-Aug-2001 12-Feb-2009 N/A due to p/n
NYGE, Saab Aerotech Aircraft Services
NYGE SB 08-06-34-03 A
EGPWS System Provision for Inhibit Unit)
30-Nov-2009 A 08-Feb-2010
NYGE SSB DR-MGPC-YELL
A 29-Nov-2006
NYGE TDM 12-22
A L35A Move mission inverter A 10-Sep-2012
NYGE TDM 12.23
Installation laser prismor L35 A 10-Sep-2012
NYGE TDM 02-25
Installation Underving-kanaler 16-Oct-2002 12-Dec-2003 LFV app.No: M21/02 revision 1.
NYGE TDM 02-26
Box 3 Installation 01-Nov-2002 03-Dec-2003 Approved in accordance with EASA 2004-11267 and with LFV AFMS S04/89 R2.
NYGE TDM 02-28
Utv. Framtagning mod.balkar LR-35 18-Nov-2002 12-Dec-2003
NYGE TDM 03-03
B Operators Console L35A 02-Apr-2007 B 26-Feb-2008 only updated to rev.B
NYGE TDM 03-07
Alkan Fairings (mod.) 27-Feb-2003 12-Dec-2003 Approved by EASA no. 235 in accordance with LFV Mod. Cert. No. M29/03.
NYGE TDM 03-17
ACAS Installation 06-May-2003 28-Oct-2004 Approved i.a.w. EASA Doc. No: STC S.A.00255
NYGE TDM 03-19
Mission Inverter Modif. 20-Nov-2003 05-Dec-2003 Approved in accordance with LFV M37/03 and EASA 1985.
NYGE TDM 03-23
U95 Installation L35A 10-Sep-2003 D 08-Nov-2005 Rev.D updated
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
26(195)
NYGE TDM 04-03
D Astor L35A 16-Jan-2004 D 21-Nov-2012 Effektindikering/Ground test
NYGE TDM 04-06
C Darts System L35A 05-Dec-2006 01-Jan-2006 Approved in accordance with DOA 21J.108,04-06.
NYGE TDM 05-06
Removal of Reflector System 30-May-2005 11-Nov-2005 Approved i.a.w. DOA 21J.108,05-06
NYGE TDM 05-15
Install. Jumpseat Intercom 18-Jul-2005 08-Dec-2005 Approved in accordance with DOA 21J.108,05-15.
NYGE TDM 05-17
GMS anpassning i nya OP-racken 26-Aug-2005 08-Dec-2005 Approved in accordance with DOA 21J.108,05-17.
NYGE TDM 05-19
Install. GPS Map and GP&C Transponder
08-Sep-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-19.
NYGE TDM 05-20
Install. Mission Equip. new OP-Console
13-Sep-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-20.
NYGE TDM 05-26
Install. Cabin Side Wall Cable Channel
20-Oct-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-26.
NYGE TDM 05-34
Install. Structural Plug FAA STC SA2479CE
11-Nov-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-34.
NYGE TDM 06-22
Re-mod. Hydraulic system 05-May-2006 15-May-2007
NYGE TDM 06-33
Robot 15 Radar Altimeter (Nav Demo Pod)
05-Jul-2006 26-Oct-2006
NYGE TDM 06-34
Meteor Proximity Fuse 05-Jul-2006 26-Oct-2006
NYGE TDM 06-36
A A100 (to carry on L35A) 23-Apr-2007 A 25-Feb-2008
NYGE TDM 08-02
C Enhanced Surveillance L35A 09-Mar-2010 C 18-Aug-2009 Original compliance to rev A of TDM. TDM rev B and C does not affect previous compliance.
NYGE TDM 08-06
C EGPWS MK.8 & Mission Inhibit System
05-Mar-2010 C 30-Oct-2008 Original compliance with rev A. Rev B and C does not affect previous compliance.
NYGE TDM 08-07
E LR35A GPS-Map Display 12-Apr-2010 E 10-Sep-2012 Compliance was IAW TDM rev B. Previous compliance not affected by rev D.
NYGE TDM 08-09
C Install termination resistors D 01-Sep-2012
NYGE TDM 08-13
A Barlast DARTS L35A 10-Mar-2008 A 10-Mar-2008
NYGE TDM 08-17
C ELT 406 L35A 04-Jul-2008 C 03-May-2010 Original compliance with TDM rev A. Rev B and C does not affect previous complaiance.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
27(195)
NYGE TDM 08-26
A Mission Antenna Adapter 28-Oct-2008 A 15-Dec-2008
NYGE TDM 09-01
C LR35A U-95 SORC Lite 24-Sep-2009 C 30-Sep-2009 Original compliance i.a.w rev B
NYGE TDM 09-30
E LR35A Removable Hard Disk Drives 30-Apr-2010 E 04-July-2012
NYGE TDM 10-04
A Overload Sensing Control 02-Jun-2010 A 14-Oct-2010 Initial complaiance was I.A.W TDM rev 2
NYGE TDM 10-27
A LR35A U95-D2 22-Apr-2010 A 15-Jun-2010
NYGE TDM 95-01
Installation Intercom 10-Jan-1995 24-Jan-1995
NYGE TDM 95-02
Modifiering Transponder-system 10-Jan-1995 24-Jan-1995
NYGE TDM 96-01
Miss-rack,GPS-antenn,CVR,inverter m.m.
12-Feb-1996 15-Mar-1996
NYGE TDM 97-01
TAPS 20-Feb-1997 01-Jan-1998
NYGE TDM 97-09
Kontrollprogram SE-DHO 26-Nov-1997 01-Jan-1998
NYGE TDM 98-06
Astor L35A 09-Mar-1998 10-Feb-1998 Approved in accordance with LFV M20/99.
NYGE TDM 98-12
Installation BRNAV L35A 26-Jun-1998 16-Apr-1998 Approved in accordance with S-CAA Approval reference LS 2005-7326.
ROCKWELL, Rockwell Collins U.K.Ltd
ROCKWELL SIL 07-1
Reply Inhibition On The Ground EASA AD 2009-0097 Rev IR
25-May-2007 18-Aug-2009 PCW Are in compliance with EASA AD2009-0097 Ref TDM03-17 DWG MF1030064-1 Rev.C
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
28(195)
1.3 GFE Aircraft Learjet 35A SE-DHP
1.3.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
Learjet
35A
075 SE-DHP 12549 8437 2012-11-23
1.3.2 Engines Type: TFE731-2-2B
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours
remaining
to MPI:
Hours
remaining
to CZI:
Left Engine P-74542 14889 11860 549 561
Right Engine P-74277 10913 7322 1051 3851
1.3.3 Avionics System: Type / Part Number: Note:
Autopilot JET FC 200
Dual VHF-COM Collins VHF-22C
HF-COM Collins 718U-5
ICS & Audio System DB System
Dual VHF-NAV Collins VIR-30A
GPS Garmin GPS 165 TSO
Dual DME Collins DME40
ADF 1 & 2 Bendix/King KDF-806
XPDR 1 & 2 Collins TDR94D Mode S
EHS
TCAS II Collins TCAS-4000
TCAS II VSI/RA/TA Indicator LH /
RH
Collins TVI-920
TAWS / EGPWS Honeywell MK VI
RDR ALT Collins ALT-55B
Weather Radar Honeywell Primus 400
MFD Display Honeywell MFRD
ELT Kanad ELT 406-AF-H
Dual Mach Airspeed indicator IDC 2680003-2
Altimeter incl. encoder LH IDC 28007-017
Altimeter RH IDC 23932-053
Altitude Report & Alerting System IDC 23989-011
Air Data Display Unit 9D-80130-32
Flight Director Indicator LH Collins 329B-7R-2
Vertial Gyro Indicator RH JET 5-4000-08
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
29(195)
Dual VG-Gyro JET VG-206EL
Standby Altitude Gyro JET AI 804
Horizontal Situation Indicator LH Collins 331A-6R
Horizontal Situation Indicator RH Collins 331A-3G
Dual RMI Collins 332C-10
Dual DG-Gyro JET DN-101D
RVSM
FDR Sundstrand 980-4100-FWUS
CVR Fairchild 93-A100-83
1.3.4 Mission System System: Description:
Fixed general installations
FR31 VHF/UHF COM Radio
AN/ARC 182 VHF/UHF COM Radio
GPS MAP System
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
KGS SPS-3052B Inverter 230VAC 50Hz
Laser Prism
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ASTOR Fixed installed system
ADRIAN C & S Pod mounted system
U95-N Pod mounted system
U95-D2 Pod mounted system
U95 Sorc Pod mounted system
A100 Pod mounted system
Missile Threat Simulator
DARTS Pod mounted system
GMS Pod mounted system
Chaff Dispenser
BOX 3 Pod mounted system
Target Towing
MTR 101 Outboard pod mounted winch
AS200 MDI (Miss Distance Indicator)
TLX Height keeping target
Precisions GPS Pos System
TAPS
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
30(195)
1.3.5 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, U95-N, U95-
D2, U95 Sorc, A100, DARTS,
GMS, BOX 3 and MTR 101
General Signal Harness General Signal Harness Two pair shielded
AWG 20 x 25
MTR 101 MTR 101 Harness MTR 101 Harness Two pair shielded
AWG 20 x 3
AWG 16 x 4 +
shield U95-N, U95-D2, U95
Sorc, A100 and GMS MIL-STD-1553B Data
Bus
MIL-STD-1553B Data
Bus
Twinax x 8
U95-N, U95-D2, U95 Sorc,
A100, DARTS and GMS AC Power
115/200VAC 400 Hz 3-
Phase 3 x 10 A
AC Power 115/200VAC
400 Hz 3-Phase 3 x 10 A
AWG 12 x 10 +
shield
Adrian C & S, GMS and BOX
3 DC Power 28 VDC 150
A
DC Power 28 VDC 150
A
AWG 4 x 4
MTR 101 Coaxial 2 x 75 Ω Coaxial 2 x 75 Ω
Adrian C & S Coaxial 3 x 50 Ω Coaxial 3 x 50 Ω
Recognition Light Recognition Light
Cable
Recognition Light Cable AWG 16 x 4 +
shield
1.3.6 Antenna layout
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
31(195)
1.3.7 Inspektion due times and dates Status date November 23
rd 2012.
Description Maint. RefC/Out date C/Out Hrs Due Hrs Due date Due Landings
Aircraft SE-DHP
Phase A 300 hour insp. AMP 2012-01-09 12407 12707 2013-02-09
Phase B 600 hour insp. AMP 2012-01-09 12407 13007 2014-02-09
Phase C 1200 hour insp. AMP 2010-11-05 12288 13488 2014-11-04
Phase D 2400 hour insp. AMP 2010-12-01 12288 14688 2018-11-29
Special operational fatigue inspect AMP 2009-02-26 11911 13111,3
12000 Hrs Inspection AMP 2001-03-26 10287,00 16287
45 days insp. AMP 2012-11-16 12547 2012-12-31
6 Month Inspection AMP 2012-08-06 12509 2013-02-06
2 Year Inspection AMP 2010-12-01 12288 2012-11-30
12 Year Airframe inspection AMP 2001-03-25 2013-03-22 13042
MPI engine zone inspecition LH AMP 2007-04-17 11653 13053,5
MPI engine zone inspecition RH AMP 2010-03-04 12186 13586,7
300 Hrs Inspection AMP 2012-01-12 12407 12707,8
1200 Hrs Inspection AMP 2008-01-15 11781 12981,9
3000 Landing Inspection AMP
6000 Major Landing Gear Inspection AMP 1998-08-19 12000
Operator's Console 300h/1y insp. AMP 2011-11-24 12400 12707 2013-02-09
ACAS 2 (TCAS) 24month insp. AMP 2011-11-24 12400 2013-11-23
Mission equipment 300 hour insp. AMP 2012-01-17 12407 12707,8
Engine S/N P-74542 Remaining
Engine 150 hrs insp. AMP 12557,8 8,3
Engine 300 hrs insp. AMP 12588,7 39,2
Engine 800 hrs insp. AMP 13299,1 749,6
Engine Compressor Zone Insp. AMP 13111,1 561,6
Engine Major Periodic Inspection AMP 13099,1 549,6
Engine S/N P-74277 Remaining
Engine 150 hrs insp. AMP 12557,8 8,3
Engine 300 hrs insp. AMP 12800,9 251,4
Engine 800 hrs insp. AMP 13000,9 451,4
Engine Compressor Zone Insp. AMP 16400,9 3851,4
Engine Major Periodic Inspection AMP 13600,9 1051,4
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
32(195)
1.3.8 Implemented Changes Status date November 23rd 2012. For abbreversions see chapter 1.2.8
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Compliance Status Remarks
AVCON, Avcon
Industries, Inc
AVCON STC SA00432WI
R Install. Avcon Fins 31-mar-05 R 12-jul-06
AVCON STC
SA2479CE
A Install. Plug of Dual Hatches 30-jun-05 A 12-jul-06
AVCON STC
ST00564WI
AFM suppl. increase T/O weight........ 25-aug-97 13-jul-06
AVCON STC
ST00611WI
C Increase Takeoff Weight to 19600
pounds
11-mar-05 C 12-jul-06
AVCON STC
ST00612WI
B Increase Wing/Tip Zero Fuel Weight 28-nov-97 B 12-jul-06
AVCON STC
ST00613WI
C Increase Landing Weight to 16000
pounds
11-mar-05 C 12-jul-06
EASA, European
Aviation Safety
Agency
EASA AD 2006-0265
Incorrect transponder altitude 30-Aug-2006
13-Nov-2009
EASA AD 2008-0159
Improve EHS Operation HONEYWELL SB MST 67A-34-56 HONEYWELL SSBMST 67A-SW5 Rev 1
25-Aug-2008
01-Dec-2010 N/A transponder P/N installed
EASA AD 2009-0097
IR Mode S Transponder -Check/Modification
DHC SB 8-34-243 Rev A EASA AD 2010-0067 ROCKWELL SIL07-1
29-Apr-2009
IR 28-Jul-2009
EASA AD 2009-0173
1 Mode S Transponder Mod/Repl 30-Sep-2010
1 08-Dec-2010 N/A due to ADC p/n
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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33(195)
EASA AD 2009-
0251-E
Portable Fire Extinguishers-
Ident/Repl
25-Nov-
2009
07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-
0262
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-
115 Rev C
15-Dec-
2009
07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-
0278
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-Dec-
2009
07-May-
2010
N/A N/A by current P/N installed
EASA AD 2010-0003
R1 Mode S Transponder -Check/Modification
11-Jan-2010
R1 10-Mar-2010
N/A due to p/n
EASA AD 2010-
0204
IR Mode S Transponder -Mod/Repl 06-Oct-
2010
IR 08-Dec-2010 N/A by ADC p/n installed
EASA AD 2012-
0237
KIDDE GRAVINER HAND OPERATTED
FIRE EXTINGUISHER
06-sep-2012
EASA STC
EASA.IM.A.S.0144
9
Install. of Dual Openable Hatches 20-feb-06 23-nov-06
FAA, U.S, Federal
Aviation
Administration
FAA, U.S AD 2000-24-19
Donning oxygen masks 22-nov-00 26-feb-03 Complied with by insert of AFM change 12
FAA, U.S AD 2001-07-11
Goodyear Flight Eagle Tire Tread Separat
LEARJET AW 32-021 01-May-2001
17-May-2001 N/A by s/n on tire
FAA, U.S AD 2001-
15-17
Prevent erroneous altitude
interpretatio
20-aug-01 12-feb-09 N/A due to p/n
FAA, U.S AD 2004-
03-08
To prev. structural damage to
eng.pylons
LEARJET SB 51-03 LEARJET SB 51-04
Rev 5
08-mar-04 09-mar-04 SB 51-04 previous carried out.
FAA, U.S AD 2005-
13-36
Detailed inspection of aileron cable. 09-aug-05 19-sep-05 Checked OK.
FAA, U.S AD 2005-
16-09
Inspection of Tip Tank Flapper Valves
Supersedes AD 95-25-03
LEARJET SB 28-10 13-sep-05 14-sep-05 Flapper p/n 2323006-802 previously installed. No
further action req.
FAA, U.S AD 2007-
04-18
Modify Standby Fuel Pump "switches" LEARJET SB 28-11 Rev 5 23-mar-07 15-mar-07 Previusly complied with. Ref. Learjet SB 28-11
FAA, U.S AD 2007-
17-17
Unsealed gaps in engine firewall 02-Oct-
2007
11-sep-07 Previously carried out, ref. SB 54-03
FAA, U.S AD 2008-02-19
HP-Turbine Disc replacement. 19-feb-08 06-feb-08 N/A due to engine model.
FAA US AD 74-08-09
3 Transport categoryairplanes equipped with lavatories
11-May-2012
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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34(195)
FAA, U.S AD 76-18-
07
Connection of Inverter to correct Bus LEARJET SB 24-03 11-dec-00 11-dec-00 This AD is carried out 1976-09-29
FAA, U.S AD 78-16-
03
To precl. a fail. of the Refr. Cond. Fan
Issued 1978-08-17
LEARJET SB 21-03 11-dec-00 11-dec-00 This AD is carried out 1978-07-30
FAA, U.S AD 79-08-
01
1 Aeronca thrust Reversers Suppl to
AFM
19-apr-82 1 13-feb-09 N/A Aeronca Thrust Reversers not installed
FAA, U.S AD 80-06-02
Starter assisted airstart 24-mar-80 03-dec-93
FAA, U.S AD 80-07-
09
Cabin Main Entrance Upper Door LEARJET AMK79-09 01-May-
1980
17-nov-80
FAA, U.S AD 80-17-
11
Airspeed Limitation Placard LEARJET SB 11-03 Rev A 28-aug-80 23-sep-80
FAA, U.S AD 80-18-
08
To Prevent loss of Emergency
electrical Power............
28-aug-80 01-jan-03 N/A due to Component p/n
FAA, U.S AD 80-19-
09
1 Motive Flow Valve LEARJET AMK80-07 LFV LVA1625
Rev A
11-dec-80 1 24-dec-80
FAA, U.S AD 80-19-
11
1 AFM insert LFV LVD1635 Rev A 20-May-
1985
1 09-feb-06 Checked. Previously complied with.
FAA, U.S AD 81-04-
06
Cockpit Voice Recorder A100 series 01-apr-81 12-feb-09 N/A due to model & s/n
FAA, U.S AD 81-13-
07
To ensure oper. without fuel
starvation
LFV LVA1748 25-jun-81 10-aug-81
FAA, U.S AD 82-01-
05
2 Stall Warning Accelerometer Check LEARJET SB 27-12 Rev B LFV
LVA1912
10-apr-86 2 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5
rev.74 och FAA AMOC från 2005-03-24
FAA, U.S AD 83-08-
03
Insp.RH Engine Hydraulic Pressure
Line for Interference.
LEARJET SB 29-01 Rev 1 03-May-
1983
19-dec-08
FAA, U.S AD 84-19-
06
To prevent Aileron/Trim Tab Flutter
due to failure of the trim tab ctrl
system
22-Oct-
1984
14-jun-85
FAA, U.S AD 84-20-
06
Inspect LH Hydraulic Lines for
Interfere superseded by 86-22-05
LEARJET SB 29-02 03-nov-86
FAA, U.S AD 85-16-
04
Airplane Lateral Control
Characteristics
FAA, U.S AD 96-19-13 LEARJET
AMK83-05 LFV LVD2034
06-sep-85 22-jan-86 N/A due to config. (STC SA766NW never been installed).
FAA, U.S AD 85-22-
10
Collins HSI & FD indicators 31-dec-85 15-jun-09 N/A by p/n & s/n
FAA, U.S AD 86-05-
05
1 Relocation of Battery Vent Inlet Fitting LEARJET SB 24-10 LFV LVD2046 19-jan-88 1 18-jun-86
FAA, U.S AD 86-22-
05
To prevent of flap operation.......... LEARJET AMK86-04 10-nov-86 03-nov-86
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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35(195)
FAA, U.S AD 87-02-
06
Insp. of Fwd. Eng.Mounts for Cracks LEARJET SB 71-03 Rev 1 06-feb-87 17-jan-05 Para.A: see Phase A3 300 hour insp. Para.B: see A/C
status RAL
FAA, U.S AD 87-04-
06
Autopilot FC-530 Limitations 09-mar-87 12-feb-09 N/A due to A/P model
FAA, U.S AD 89-12-
01
Inspection of Drag Chute Riser LEARJET SB 25-07 Rev A 03-jul-89 07-dec-10 N/A N/A by Riser P/N installed
FAA, U.S AD 91-03-08
Deactivation of Forward Cabinet and Overhead Fluoriscent Light Circuits
LEARJET SB 33-05 Rev A 12-feb-91 19-dec-08
FAA, U.S AD 92-19-
12
SYSTEM TUBE (W-IN 30D) LEARJET AMK90-05 17-nov-92 15-feb-93
FAA, U.S AD 95-19-
04
1 Omega Navigation System 27-mar-00 1 03-dec-10 N/A AD note cancelled
FAA, U.S AD 95-20-
03
Insp.of Cabin Pressurization
Outflow....
LEARJET SB 21-19 02-nov-95 02-dec-95
FAA, U.S AD 95-22-
01
ALC Series 66 fluorescent lamps 07-Aug-2012
FAA, U.S AD 95-25-
03
Inspection of Tip Tank Flapper Valves LEARJET SB 28-10 27-dec-95 14-feb-96
FAA, U.S AD 96-19-
13
Raisbeck Group STC SA766NW FAA, U.S AD 85-16-04 LEARJET
AMK83-05
22-Oct-
1996
22-jan-86 N/A due to config. (STC SA766NW never been installed).
FAA US AD 97-05-
03
1 GNS XLS and GNS XL system 1-Nov-2011
FAA, U.S AD 98-06-
28
Electrical Arcing and Fire Hazard LEARJET SB 21-24 Rev 1 24-apr-98 09-dec-08 N/A due to s/n
FAA, U.S AD 98-25-
10
1 Inspection of seat restraint system LFV LVD2929 Rev 2 14-jan-00 1 03-dec-10 N/A Affected seat belts not installed
FAA, U.S AD 99-08-
21
Oxygens Masks 02-jun-99 19-dec-08 N/A due to different cure date
FAA, U.S AD 99-23-
19
Replacement or Spoiler Actuator LEARJET SB 27-36 28-Oct-
1999
09-dec-08 N/A due to s/n
FLIGHT INT, Flight
international inc
FLIGHT INT STC
SA1604SO
Hard points 26-nov-99 22-May-1989
KEITH, Keith
Products, Inc
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
36(195)
KEITH SB 163 B Load Shed Installation 19-nov-99 B 17-apr-07
KEITH SB 166 A Belt Guard Installation 08-Oct-
2001
A 17-apr-07
KEITH STC
ST09366SC
Install. of Electric-Driven Vapor A/C 12-aug-97 06-aug-99
LEARJET,
Bombardier,
LEARJET
LEARJET AAK 71-13 F Gravel Runway Operations Kit 10-sep-99 F 27-mar-01
LEARJET AAK 76-03 WING ICE L. 30-jun-76 11-May-1989
LEARJET AAK 79-02 PITOT HEAT IND. 30-jun-79 03-jul-81
LEARJET AAK 79-04 CONICAL FAN SPINNER 30-jun-79 22-apr-89
LEARJET AAK 80-02 INCREASE T.O. WEIGHT 30-jun-80 15-nov-84
LEARJET AAK 80-03 INCREASE LAND.WEIGHT 30-jun-80 02-dec-88
LEARJET AAK 81-01 1 Starter Contactor 30-jun-08 1 16-sep-08 PCW
LEARJET AAK 82-02 1 Install. Cabin Temp.Contr.Syst.filters 01-Oct-1982
1 08-mar-06 N/A N/A by s/n
LEARJET AAK 83-06 VERT.STAB. ACCESS 30-jun-83 29-jul-84
LEARJET AAK 83-08 Inst.of Comp.to allow variable Pitch Trim Settings at takeoff
08-mar-85 28-nov-01 Checked. Previously complied with.
LEARJET AAK 84-03 A WINDSHIELD HEAT 30-jun-84 A 12-mar-85
LEARJET AAK 86-02 1 Inst. of LDG Actuator Down Lock
Switch
22-sep-08 1 04-nov-08 Checked PCW.
LEARJET AAK 89-04 D Inst. of Doublers at Frame 7 11-aug-95 D 27-mar-01
LEARJET AAK 89-14 25 DG.FLAP LIMIT SWITCH 30-jun-89 02-May-1990
LEARJET AAK 90-12 1 Inst. of Batting at Wing Spar 1 Splice 22-sep-08 1 04-nov-08 Checked PCW.
LEARJET AAK 90-16 IR Overhead Fluorescent Light. Wiring Prov.
30-jan-91 IR 10-mar-09
LEARJET AAK 91-05 1 Inst of Defog Temperature Sensors 16-feb-09 1 05-jun-09 N/A Due to Electric Windshield not installed
LEARJET AMK 76- A WING SKIN FASTENERS 30-jun-76 A 14-dec-79
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2012-12-06
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02
LEARJET AMK 76-
07
1 CABIN AIR CONTR.VALVE 30-jun-76 24-dec-77
LEARJET AMK 76-
09
A OIL PRES. TRANSM. 30-jun-76 A 24-dec-77
LEARJET AMK 77-
01
AIL.CABLE PULLEY 30-jun-77 24-dec-77
LEARJET AMK 77-
03
ENGINE BLEED AIR VALVE 30-jun-77 24-dec-77
LEARJET AMK 77-
06
A WING BOLTS 30-jun-77 A 24-dec-77
LEARJET AMK 77-08
ESS.BUS C/B PANEL 30-jun-77 24-dec-77
LEARJET AMK 78-04
ENGINE BLEED AIR DUCT 30-jun-78 23-feb-86
LEARJET AMK 78-06
A ENGINE BLEED AIR TUBE 30-jun-78 A 08-nov-79
LEARJET AMK 78-08
A GENERATOR DRIVE SPLINES DRIVE SHAFT
30-jun-78 A 19-jun-85
LEARJET AMK 78-12
A ENGINE BLEED AIR PLUMBING 30-jun-78 A 15-jan-80
LEARJET AMK 78-13
A ESS.BUS 04-jun-07 A 11-sep-07 Previously carried out, ref. AMK 78-13
LEARJET AMK 79-09
CAB.DOOR MECHANISM (AD800709) (AD800709)
FAA, U.S AD 80-07-09 LFV LVA1613 30-jun-79 17-nov-80
LEARJET AMK 79-10
ENGINE FUEL TUBE 30-jun-79 12-jul-80
LEARJET AMK 79-11
AILERON DRAIN 30-jun-79 17-nov-80
LEARJET AMK 80-
01
B RUDDER PEDAL 30-jun-80 B 03-aug-81
LEARJET AMK 80-
06
A ENG.MOUNT (AD801711) (AD801711) 30-jun-80 A 15-apr-81
LEARJET AMK 80-
07
MOTIVE FLOW VALVE (AD801909)
(AD801909)
FAA, U.S AD 80-19-09 Rev 1 LFV
LVA1625 Rev A
30-jun-80 24-dec-80
LEARJET AMK 80-
17
1 Installation of Current Limiter
Warning
28-jun-10 A 04-jul-08 Starter engage lamps, moved to opt. position
LEARJET AMK 81-
17
HOR.STAB. HINGE PIN 30-jun-81 23-mar-86
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LEARJET AMK 83-
03
AILERON TRIM TAB BALANCE WEIGHT
(AD84190 (AD84190
30-jun-83 14-jun-85
LEARJET AMK 83-
05
WING STALL STRIP (AD851604)
(AD851604)
FAA, U.S AD 85-16-04 FAA, U.S AD
96-19-13
30-jun-83 22-jan-86 N/A due to config. (STC SA766NW never been installed).
LEARJET AMK 84-
08
SPOILER SYSTEM 30-jun-84 23-mar-86
LEARJET AMK 85-01
A POWER DIST. 30-jun-85 A 23-mar-86
LEARJET AMK 86-
04
WING FLAP SECTOR (AD862205)
(AD862205)
FAA, U.S AD 86-22-05 30-jun-86 03-nov-86
LEARJET AMK 90-
05
SYSTEM TUBE (AD921912)
(AD921912)
FAA, U.S AD 92-19-12 09-Oct-
1991
25-jan-93
LEARJET AW 32-
021
Goodyear Flight Eagle Tire Tread
Separat
FAA, U.S AD 2001-07-11 05-feb-01 17-May-2001 N/A by s/n on tire.
LEARJET SB 00-01 Inspection/Replacement of cables 27-feb-01 26-mar-01
LEARJET SB 05-01 FIRE EXT. BOTTLE (HYDROST.) 18-nov-92 18-nov-92
LEARJET SB 11-02 AIRSPEED LIMIT PLACARDS 06-dec-76 02-jan-77
LEARJET SB 11-03 A AIRSPEED LIMIT PLACARDS AD841906 FAA, U.S AD 80-17-11 18-sep-80 A 23-sep-80
LEARJET SB 11-04 WASTE DISP.REC. PLACARDS
AD740809
18-dec-81 25-jul-91 N/A due to model and s/n.
LEARJET SB 11-05 CREW SEAT BELT PLACARDS 31-aug-83 23-Oct-1983
LEARJET SB 11-06 BATTERY PLACARDS 21-jul-87 25-jul-91 N/A due to SB32-04 is carried out.
LEARJET SB 11-07 ID PLATE (O) 06-nov-92 23-jul-93
LEARJET SB 11-10 Repl.of Fuel Servicing Placards 17-dec-01 06-feb-04
LEARJET SB 21-02 Cabin Air Distribution 02-May-
1977
25-jul-91 N/A. Optional.
LEARJET SB 21-03 CONDENSER FAN ASSY. AD781603 FAA, U.S AD 78-16-03 12-jul-78 30-jul-78
LEARJET SB 21-04 Inst. of Refrigeration
Syst.Warn.Placard
22-feb-79 23-May-1979
LEARJET SB 21-05 CABIN PRES. SAFETY VALVE 18-dec-79 05-May-1980
LEARJET SB 21-06 Insp.of Air Distr.Sleeves & Clamps-
Tailc
23-sep-80 16-nov-80
LEARJET SB 21-07 CABIN PRES. SAFETY VALVE
(CHANGED) Garrett SB 5-2290
28-Oct-
1980
29-jan-81
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2012-12-06
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LEARJET SB 21-14 1 OUTFLOW VALVE SAFETY VALVE (R) 03-jan-95 1 22-dec-95 Superseded by SB 21-19.
LEARJET SB 21-15 2 Repl. of Refrig.Syst. Press Switch 22-jul-05 2 11-Oct-2005 N/A to Keith R34.
LEARJET SB 21-18 3 Imp.W-shield Aux.Defog & Aux.Crew Heat
11-aug-08 3 04-nov-08 N/A N/A due to AAK86-1 not incorporated
LEARJET SB 21-19 Insp.of Cabin Press.Outflow & Safety Vlv 130406-21-A4011 R2,102850-21-A4021 R2
FAA, U.S AD 95-20-03 03-jan-95 22-dec-95
LEARJET SB 21-24 1 Repl.of Aux.Cabin Heater Wiring FAA, U.S AD 98-06-28 13-aug-96 1 09-dec-08 N/A due to s/n
LEARJET SB 21-25 3 Inst.of Improved Refrigeration
Comp.Asse
12-nov-07 2 06-feb-08 N/A Due to Keith Aircondition System TR-134 Installed
LEARJET SB 21-26 5 Mod.of Auxiliary Cabin Heather 16-May-
2007
5 05-Mar-2012
LEARJET SB 22-02 Sec.Yaw Damper Servo Cable Clamp Bolt
06-sep-78 10-mar-78
LEARJET SB 22-03 Repl.of Yaw Damper Servo Sector Bolts
02-feb-79 03-jun-79
LEARJET SB 22-04 C Mod. of Mach Trim Computer J.E.T SB 501-1132-9E, -10B, -11
25-mar-80 C 01-sep-91 N/A
LEARJET SB 22-05 Mod.of FC-530/-535 Autopilot Computer
05-jan-87 25-jul-91 N/A N/A due to A/P model
LEARJET SB 22-07 3 Inst.of Autopilot Accelerometer Monitor
11-jun-07 2 29-May-2007 N/A AAK 83-2 not complied with.
LEARJET SB 23-03 2 Increased FOD Protection-Installation of Antenna Protection.
09-jul-01 2 11-jan-06 Previous revision carried out.
LEARJET SB 24-03 AC Inverter Excitation & Control
Check
FAA, U.S AD 76-18-07 09-aug-76 29-sep-76
LEARJET SB 24-04 A Reloc.of AC
Second.Inv.Ground.Connection
01-jun-77 A 24-dec-77
LEARJET SB 24-05 Repl.of Generator Bearings Bendix SB
R-358 & Suppl No.1
02-May-
1978
27-jul-78
LEARJET SB 24-06 Insp.of Battery Vents for Obstruction 29-sep-80 25-jul-91 N/A Found not applicable due to incorporation of SB 24-
15.
LEARJET SB 24-07 Current Limiter Box Moisture Proofing 15-jan-81 25-jul-91
LEARJET SB 24-08 Insp.of No.4 Gauge Electrical Cables 11-May-
1982
25-jul-91
LEARJET SB 24-09 Insp.Fuses for Proper Prot.Covering &
PN
19-apr-83 25-jul-91
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LEARJET SB 24-10 Reloc.of Battery Vent Inlet Fitting
AD860505
FAA, U.S AD 86-05-05 Rev 1 18-Jul-
1985
18-jun-86
LEARJET SB 24-11 Add.of Ret.for Gen.Warn.Ctrl
Box.Connect
01-nov-90 25-jul-91
LEARJET SB 24-15 1 Inst.of Concorde Sealed Lead-Acid
Batt.
24-mar-08 1 04-sep-08 PCW
LEARJET SB 25-03 Insp.of Drag Chute Mechanism Bolt 10-nov-80 09-jun-81
LEARJET SB 25-04 A Insp.of Drag Chute Mech.for Proper
Clear
11-nov-81 A 15-aug-82
LEARJET SB 25-06 Insp.Drag Chute Canister Lid Latch
Screw
19-feb-87 25-jul-91
LEARJET SB 26-02 A Verif.& Ident.of Eng.Fire Ext.Bottl.Wire
30-apr-91 A 25-jul-91
LEARJET SB 26-03 2 Repl. of Fire extinguishing Bottle Ass. 20-aug-07 2 21-jan-08 Carried out at L/H side
LEARJET SB 26-04 1 Engine Fire Element Insp./repl. 11-aug-08 1 04-nov-08 N/A N/A by s/n on elements
LEARJET SB 27-05 Stall Warn.Computer Plug &
Receptacle ID
13-sep-76 31-dec-76
LEARJET SB 27-06 Insp.of Alt.Pressure Switch Wiring 06-May-
1977
27-dec-77
LEARJET SB 27-07 Mod.of Spoileron Computer Assembly
J.E.T SB 501-1133-4
01-Oct-
1977
12-mar-85
LEARJET SB 27-08 Wiring of Pilot & Copilot Cntrl Wheel.. 24-May-
1978
13-dec-81
LEARJET SB 27-09 Insp.of Wing Flap Actuators 19-dec-78 25-jul-91
LEARJET SB 27-10 Rework of Pilot/Copil.Ctrl Wheel Trim
..
19-apr-79 01-jul-80
LEARJET SB 27-11 Insp.of Aileron for Drain Holes 06-nov-79 27-dec-79
LEARJET SB 27-12 B Stall Warn.Accelerometer Op.Check FAA, U.S AD 82-01-05 Rev 2 LFV
LVA1912
25-sep-81 B 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5
rev.74 och FAA AMOC från 2005-03-24
LEARJET SB 27-14 Insp.of Welds on Rudder Pedal
Supp.Assy
08-sep-83 27-mar-84
LEARJET SB 27-16 Insp.Flap Attach.Fittings for Cracks 27-May-
1986
03-nov-86
LEARJET SB 27-24 Insp.of Ail.& Rudder Ctrl Cable Assy Ter
08-nov-93 01-dec-93
LEARJET SB 27-33 Removal of Sealant from Aileron Rib 27-May-1997
19-feb-98
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2012-12-06
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LEARJET SB 27-35 4 Inst.of Secondary Locking Feature 15-aug-03 4 03-nov-03 Previous rev. carried out.
LEARJET SB 27-36 Replacement of Spolier Actuator FAA, U.S AD 99-23-19 14-dec-98 09-dec-08 N/A due to s/n
LEARJET SB 27-40 6 Insp/Inst. of Flap Structure Components
16-aug-10 6 10-Nov-2011 PCW Previous revision carried out
LEARJET SB 27-43 Recalibration rosemount 19-jan-05 17-mar-05 N/A due to STC ST00321WI-D not complied with.
LEARJET SB 27-45 1 Insp. Spoiler panels 29-Mar-2012
LEARJET SB 28-02 INAKTIV
Insp.of Tip Tank Elect.Conduit for Damag
20-feb-76 03-jan-77
LEARJET SB 28-04 Reloc.of Fuel Probes on Wing Tank Access
01-nov-77 20-sep-79
LEARJET SB 28-05
INAKTIV
Op.check of Fuel Jettison Valves 14-feb-80 07-sep-80
LEARJET SB 28-06 Insp.of Rec.for Field Rep.of Mot.Flow
Vl
21-aug-80 24-sep-80
LEARJET SB 28-08 Insp.of Motive Flow Vlv Shroud Cover 27-aug-90 09-jan-91
LEARJET SB 28-10 Inspection of Tip Tank Flapper Valves FAA, U.S AD 2005-16-09 FAA, U.S AD 95-25-03
06-Oct-1995
14-sep-05 Flapper p/n 2323006-802 previously installed. No further action req.
LEARJET SB 28-11 5 Inst.of Standby Fuel Pump Annunciators
FAA, U.S AD 2007-04-18 28-sep-09 5 26-feb-10 Rev. 1-4 PCW. AFM cheched for Change 14
LEARJET SB 28-14 2 Repl.of Tip Tank Flapper Valves 09-May-2001
2 31-aug-01 SB previuos installed.
LEARJET SB 28-18 Insp./Repl. of Fuel Filter Elements 24-aug-09 30-Oct-2009 N/A due to filter p/n
LEARJET SB 29-01 1 Insp.RH Eng.Hydr.Press.Line for Interfer
FAA, U.S AD 83-08-03 10-sep-96 1 19-dec-08 due to remod. hyd.syst.
LEARJET SB 29-02 Insp.LH Eng.Hydr.Lines for Interference
FAA, U.S AD 84-20-06 15-jun-83 14-aug-83
LEARJET SB 29-05 Repl.of Hydr.Reservoir Sight Glass Assy
07-Oct-1992
23-jul-93 N/A
LEARJET SB 30-10 1 Repl. of Wing Anti-Ice Transverse Duct 12-feb-99 1 08-dec-99
LEARJET SB 30-11 3 Inst.of High Current Capacity Wire 05-May-2008
3 04-sep-08 PCW
LEARJET SB 31-01 Repl.of Oil Press.Annunciator Cap Assy
26-Oct-1992
01-dec-93
LEARJET SB 32-03 Insp.of LG Brake & Torque Link for Inter
25-aug-81 25-jul-91
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LEARJET SB 32-04 Repl.of LG Hydraulic Selector Valve 23-jan-89 09-jan-91
LEARJET SB 32-07 1 Inst.of MLG Lower Torque Arms 10-nov-95 1 31-Oct-2003
LEARJET SB 32-18 Inst.of Main Landing Gear Wheel Screens
19-jan-99 15-mar-99 N/A. Affected Wheel Assy not installed.
LEARJET SB 32-20 Repl.of Landing Gear Shuttle Valve 09-mar-00 30-jun-00 N/A Found N/A to Part Number.
LEARJET SB 32-21 Repl.of Brake Valve Adjustment Screw 01-May-2000
26-mar-01
LEARJET SB 32-23 1 Mod landing gear squat switch wiring 09-apr-07 1 29-May-2007 N/A Previously carried out
LEARJET SB 32-26 Insp/Repl of the Nose Gear Wheel Assy
18-jan-10 10-May-2010 N/A by s/n
LEARJET SB 32-27 IR Sealant on Anti-Skid Solnoid 14-Jun-2011
LEARJET SB 33-01 Add.of Drain Holes in Tip Tank Nose Cone
03-jan-77 11-feb-77
LEARJET SB 33-03 Insp.& Mod. of LH Fwd Cabinet Light Assy
24-apr-85 25-jul-91 N/A N/A due to interior config.
LEARJET SB 33-05 A Deactiv.of Fwd Cabinet & Overhead Light. AD901406
FAA, U.S AD 91-03-08 21-dec-90 A 19-dec-08
LEARJET SB 33-06 A Activ.of Fwd Cabinet & Overhead Fluore..
12-apr-91 A 26-feb-09
LEARJET SB 34-04 Insp.of Static Ports 11-jun-82 25-jul-91
LEARJET SB 35-01 Insp.of Oxygen Mask Microphone Jack Wiri
09-sep-77 25-jul-91
LEARJET SB 35-04 Replacarding Oxygen Bottle Shutoff Valve
27-feb-04 04-aug-04 Placards installed.
LEARJET SB 36-02 A Insp.& Repl.of Eng.Bleed Air Flex Tube..
25-May-1978
A 01-sep-91
LEARJET SB 36-03 Repl Air Bottle & Weight-Balance Change
14-dec-09 11-mar-10 Due to weighing after installation of bottle p/n 6600194-6
LEARJET SB 51-01 Insp.Baggage Comp.Struct. for
Corrosion AD 84-12-03
18-jul-85 06-sep-85
LEARJET SB 51-03 Insp.of Forward Engine Beam Shear
Web.
FAA, U.S AD 2004-03-08 01-feb-01 1200H 06-sep-01 N/A N/A due to SB 51-04 performed.
LEARJET SB 51-04 5 Rep.of Forward Engine Beam Shear
Web
FAA, U.S AD 2004-03-08 12-Oct-
2009
5 11-mar-10 No rework required
LEARJET SB 51-4 3 20-jan-05 No rework req.
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2012-12-06
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LEARJET SB 52-02 Adj.of Lwr Cabin Door Hok Act.Toggle
Sw.
09-aug-77 14-jun-85
LEARJET SB 52-04 Mod.of Access Door Lock Assemblies 16-apr-79 25-jul-91 N/A Found N/A. No locks installed.
LEARJET SB 52-05 Insp.of Cabin Int.Liner-Areas Of
Emerg..
04-nov-80 25-jul-91
LEARJET SB 52-06 Mod.of Lwr Cabin Door Hook
Mechanism
18-dec-92 01-dec-93
LEARJET SB 52-10 1 Repl.of Upper Cabin Door Torsion Bar
Arm
03-jun-99 1 20-sep-99 N/A. 24 inch door not installed.
LEARJET SB 53-01 Inst.of Rivets at Fwd Eng.Beam &
Frame24
27-apr-77 01-sep-91 N/A
LEARJET SB 53-07 Inspect for Tailcone Drains 18-dec-92 01-dec-93
LEARJET SB 53-08 Inst.of Nutplates on Circ.Br.Panel
Suppo
14-feb-94 15-dec-94
LEARJET SB 53-10 1 Repl.of LowerStinger & Ventral Fin
Skin
17-mar-08 1 14-May-2008 N/A Due to Avcon Fins STC ST00432WI
LEARJET SB 53-11 3 Mod.of Tailcone Ballast Weight
Installat
01-jun-09 3 08-jan-10 Ballast not/never installed
LEARJET SB 53-13 Insp. Intern. baggage comp. floor splice
16-jan-06 08-mar-06 N/A Due to S/N
LEARJET SB 54-01 Insp.for Silicon Firesleeve-Start&Gen Ca
11-jun-82 25-jul-91
LEARJET SB 54-03 Insp/Firewall Sealing Modification 16-mar-01 17-apr-07 L/H side carried out
LEARJET SB 54-04 Insp/Repl.of Upper and Lower Pylon Skins
08-aug-01 22-mar-02 N/A by s/n on aircraft.
LEARJET SB 55-01 Insp.Horiz.Stab.Hinge Assy for Cracks 16-aug-91 16-aug-91 N/A No Thrust Reversers installed.
LEARJET SB 55-04 2 Inst.of Doublers on Horiz.Stabili.Skin 23-feb-09 2 10-jun-09 PCW
LEARJET SB 55-05 Imp.of Horiz.Stabilizer Actuator
Access
16-jan-98 30-Oct-1998
LEARJET SB 55-06 Mod.of Navigation Light Wiring
Conduit
30-aug-04 30-nov-04
LEARJET SB 71-01 Insp.for Interf.between LH Eng Starter
&
08-sep-76 02-jan-77
LEARJET SB 71-02 Eng.Firewall Sealing at Feed-Thru Condui
13-May-1982
25-jul-91
LEARJET SB 71-03 1 Insp.of Fwd Eng.Mounts for Cracks FAA, U.S AD 87-02-06 10-feb-95 1 27-jan-97
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2012-12-06
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LEARJET SB 71-05 2 Repl.of Fwd Eng.Mount Bolts 18-jun-93 2 10-jan-95 Bolt replaced L/H side w/o C00454 1997-01-21.
LEARJET SB 76-01 B Insp.of Eng. I.T.T. Cable Connectors 07-nov-83 B 27-sep-84
LEARJET SB 80-02 A Repl.of Starter Rly Cover & Magnetic Cor Bendix SB R-352A, R-355
04-mar-77 A 18-sep-79
LEARJET SB A27-42 Insp/Repl.of Aileron Ctrl Cables 23-dec-02 11-jan-03 1ea: cable effective by cal.time, inspected OK.
LEARJET SB A32-15 1 Insp.of Landing Gear Actuator Pistons 21-apr-97 1 19-feb-98
LEARJET SSK 981 Repl. of Spoiler Act. Support Bracket 19-dec-86 27-mar-01
LEARJET SSK 993 2 Repl. of Landing Gear Wheel Bearings 21-jan-91 2 08-jan-98
LFV,
Luftfartsverket
LFV LVA 1613 Modifiering av övre kabindörr LEARJET AMK79-09 27-May-
1980
17-nov-80
LFV LVA 1625 A Till,gg i flyghandbok. T,thetskontroll FAA, U.S AD 80-19-09 Rev 1
LEARJET AMK80-07
23-jun-80 A 24-dec-80
LFV LVA 1748 Revision av Flyghandbok.
Br,nslem,ngd
FAA, U.S AD 81-13-07 24-aug-81 10-aug-81
LFV LVA 1912 Periodisk kontroll av Stallvarning. FAA, U.S AD 82-01-05 Rev 2 LEARJET SB 27-12 Rev B
10-nov-83 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24
LFV LVD 1635 A Revision Flyghandbok/kontr. A/P & mod.
FAA, U.S AD 80-19-11 Rev 1 15-jul-85 A 28-sep-09 PCW Ref. FAA AD 80-19-11 R1
LFV LVD 2034 Reducering av MMO FAA, U.S AD 85-16-04 30-aug-85 22-jan-86 N/A due to config. (STC SA766NW never been installed).
LFV LVD 2046 Kontroll av batterihållare FAA, U.S AD 86-05-05 Rev 1 25-
Nov-1985
18-jun-86
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13
CHPT 9
23-May-
1991
25-jul-91 checked OK.
LFV LVD 2853 Periodisk funktionskontroll av
nödutgång
23-mar-98 02-dec-10
LFV LVD 3148 Modif. Transponder kontrollpanel 17-aug-01 12-feb-09 N/A due to p/n
NYGE, Saab
Aerotech Aircraft
Services
NYGE SB 08-06-34- A EGPWS System Provision for Inhibit 30-nov-09 A 04-mar-10
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45(195)
03 Unit)
NYGE TDM 02-20 GMS Prototyp 27-aug-02 05-jun-04 utf. i samband med Kapsel-mod.
NYGE TDM 02-25 Installation Underving-kanaler 16-Oct-2002
10-nov-03 LFV app.No: M21/02 revision 1.
NYGE TDM 02-26 Box 3 Installation 01-nov-02 29-sep-03 Approved in accordance with EASA 2004-11267 and with LFV AFMS S04/89 R2.
NYGE TDM 02-28 Utv. Framtagning mod.balkar LR-35 18-nov-02 10-nov-03
NYGE TDM 03-03 B Operators Console L35A 02-apr-07 B 26-feb-08 only updated to rev.B
NYGE TDM 03-07 Alkan Fairings (mod.) 27-feb-03 10-nov-03 Approved by EASA no. 235 in accordance with LFV Mod. Cert. No. M29/03.
NYGE TDM 03-17 ACAS Installation 06-May-
2003
30-nov-04 Approved i.a.w. EASA Doc. No: STC S.A.00255.
NYGE TDM 03-19 Mission Inverter Modif. 20-nov-03 05-nov-03 Approved in accordance with LFV M37/03 and EASA
1985.
NYGE TDM 03-23 U95 Installation L35A 10-sep-03 D 10-mar-06 Rev.D updated
NYGE TDM 04-03 D Astor L35A 16-jan-04 D 21-Nov-2012
NYGE TDM 04-06 C Darts System L35A 05-dec-06 01-jan-06 Approved in accordance with DOA 21J.108.04-06.
NYGE TDM 05-06 Removal of Reflector System 30-May-2005
02-jun-06 Approved i.a.w. DOA 21J.108.05-06
NYGE TDM 05-15 Install. Jumpseat Intercom 18-jul-05 23-nov-06 Approved in accordance with DOA 21J.108.05-15A
NYGE TDM 05-19 Install. GPS Map and GP&C
Transponder
08-sep-05 23-nov-06 Approved in accordance with DOA
NYGE TDM 05-20 Install. Mission Equip. new OP-
Console
13-sep-05 23-nov-06 Approved in accordance with DOA 21J.108.05-20A
NYGE TDM 05-26 Install. Cabin Side Wall Cable Channel 20-Oct-
2005
23-nov-06 Approved in accordance with DOA 21J.108.05-26A
NYGE TDM 06-22 Re-mod. Hydraulic system 05-May-
2006
07-nov-06
NYGE TDM 06-36 A A100 (to carry on L35A) 23-apr-07 A 25-feb-08
NYGE TDM 08-02 C Enhanced Surveillance L35A 09-mar-10 C 28-jul-09 Original compliance to rev A of TDM. TDM rev B and C does not affect previous compliance.
NYGE TDM 08-06 C EGPWS MK.8 & Mission Inhibit System 05-mar-10 C 04-jul-08 Original compliance with rev A. Rev B and C does not affect previous compliance.
NYGE TDM 08-07 E LR35A GPS-Map Display 12-apr-10 E 28-Aug-2012 Compliance was IAW TDM rev A. Previous compliance not affected by rev D.
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NYGE TDM 08-09 C Install Termination resistor C 01-09-2012
NYGE TDM 08-13 A Barlast DARTS L35A 10-mar-08 A 10-mar-08
NYGE TDM 08-17 C ELT 406 L35A 04-jul-08 C 04-jul-08 Original compliance with TDM rev A. Rev B and C does not affect previous complaiance.
NYGE TDM 08-26 A Mission Antenna Adapter 28-Oct-2008
A 22-dec-08
NYGE TDM 09-30 E LR35A Removable Hard Disk Drives 30-apr-10 E 04-July-2012 Original compliance was i.a.w TDM rev A. Rev B
does not affect previous installation.
NYGE TDM 10-04 B Overload Sensing Control 02-jun-10 B 28-Sep-2012
NYGE TDM 10-27 A LR35A U95-D2 22-apr-10 A 15-jun-10
NYGE TDM 10-31 A Overload Sensing Control Provisions 01-jul-10 A 06-jul-10
NYGE TDM 12-22 A L35A Move mission inverter A 28-Sep-2012
NYGE TDM 12-23 A Installation laser prismor L35 A 28-Sep-2012
NYGE TDM 95-01 Installation Intercom 10-jan-95 16-jan-95
NYGE TDM 95-03 Modifiering Transponder-system 06-feb-95 16-jan-95
NYGE TDM 96-04 Miss-rack,GPS-antenn,CVR,inverter m.m.
12-feb-96 15-mar-96
NYGE TDM 97-01 TAPS 20-feb-97 01-jan-98
NYGE TDM 98-06 Astor L35A 09-mar-98 27-apr-98
NYGE TDM 98-12 Installation BRNAV L35A 26-jun-98 31-May-1998
NYGE TDM 98-13 Kontrollprogram SE-DHP 26-jun-98 15-aug-98
ROCKWELL,
Rockwell Collins
U.K.Ltd
ROCKWELL SIL 07-1
Reply Inhibition On The Ground EASA AD 2009-0097 Rev IR 25-May-2007
28-jul-09
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2 GFE Aircraft Mitsubishi MU-2
2.1 Mitsubishi MU-2 Aircraft Maintenance Program
2.1.1 Comprehensive description of Mitsubishi Maintenance Requirements Manual (MR-0178-2):
The maintenance is (according to Mitsubishi Maintenance Requirements Manual MR-0178-
2.) divided into 100 hours intervals between each periodic inspection.
Some inspections have both flight time and calendar time limitations; they must be complied
with when the first limitation becomes due. For maintenance planning purpose, a "Window
For Compliance" can be established for each inspection. An inspection accomplished within
the window, will be considered as if it was completed at the flight time or calendar time due.
It is not allowed to accumulate the time between inspections.
Inspection list according to Mitsubishi Maintenance Requirements manual MR-0178-2:
• 100 Hrs/12 Month
• 200 Hrs/12 Month
• 600 Hrs/36 Month
• 1000 Hrs
• 1200 Hrs
• 1800 Hrs
• 2000 Hrs
• 1 Year
• 2 Year
• 10 Year
• Detailed and General Engine Inspection
2.1.2 Modifications that affects the maintenance program If no individual reg. numbers are mentioned, the information applies for all six individuals.
• The fuselage is modified with a hatch, which enables deployment and changing Soft
Sleeve Targets during the flight.
• An inboard hydraulic driven winch - Air Target MBV-7 Mk II - is installed. (SE-
GHD, SE-IOV and SE-IUA).
• An aircraft hydraulic system, which consists of a hydraulic oil tank installed in the
centre wing leading edge, an engine driven hydraulic pump installed on the left engine
and a shut off valve installed in the left wing leading edge, has been installed in order
to supply the inboard winch with necessary hydraulic power for operation. (SE-GHD,
SE-IOV and SE-IUA).
• One retractable launcher arm for sleeve targets is installed under the fuselage. (SE-
GHD, SE-IOV and SE-IUA).
• A set of Laser Reflector Prisms is installed on the fuselage. (SE-GHD, SE-IOV and
SE-IUA)
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• The wings have been modified with hard points to carry external under-wing stores
• The nose radome and wing tip tanks have been modified with radome covering
antennas for the inboard ECM-system ASTOR. (SE-GHA, SE-GHB and SE-GHF).
• To supply the ECM equipment, a 3-face AC, 3kVA inverter system has been installed
in the inboard aft baggage area.
• An operator console is installed in the cabin with equipment to operate the winch and
ECM units, including a set of surveillance equipment as TV-camera, mirrors etc.
• On airplanes modified with ECM System, the R/H steering wheel is removed by
installation of operator’s work station. (SE-GHA, SE-GHB, SE-GHD and SE-GHF).
• AMOC Approval: EASA.A.AMOC.01276. Exemption from installation of
Rosemount ice-detector in accordance with JCAB TCD4529-97 and MHI SB217.
2.1.3 Maintenance Documentation Maintenance of the aircraft is conducted according to the following documentation:
• Mitsubishi Maintenance Requirement Manual MR-0178-2
• Honeywell MM 72-01-32 applicable to TPE331-6-252M
• Honeywell SB TPE331-72-0404 applicable to TPE331-6-252M
• Honeywell SB TPE331-72-0019
• Hartzell SL 61-61Y
2.1.4 Guiding documents to be used during maintenance:
• Mitsubishi Maintenance Manual YET 68035
• Mitsubishi Maintenance Manual YET 71370
• Mitsubishi Maintenance Manual YET 74132
• Mitsubishi Illustrated Parts Catalogue YET 68036B
• Mitsubishi Illustrated Parts Catalogue YET 72092A
• Mitsubishi Illustrated Parts Catalogue YET 74134A
• Mitsubishi Structural Repair Manual YET 72035A
• Mitsubishi Airplane Flight Manual
• Mitsubishi Pilot Operating Manual
• Mitsubishi Service Bulletins, -Recommendations, -Letters
• Honeywell TPE331 Service Bulletins. -Recommendations. –Letters
• Saab AB TVO
• Saab AB TDM
2.1.5 Maintenance Tasks related to changes The following maintenance tasks are not included in the aircraft manufactures’ maintenance
manual. The tasks need to be included in the operators AMP:
• Launcher Arm 3 months inspection
• Launcher Arm 100 hours inspection
• Provisions for Special Mission. 1 year inspection
• Special Operational Fatigue Inspection 1000 hours
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2.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines:
• Requirements in BCL-M4.3
• FAA Airworthiness Directives
• JCAB Airworthiness Directives
• EASA Airworthiness Directives
• LVD Swedish Airworthiness Directives.
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2.2 GFE Aircraft Mitsubishi MU-2 SE-GHA
2.2.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
MU-2B-20 283 SE-GHA 10586 5954 2012-11-23
2.2.2 Engines Type: Honeywell TPE331-6-252M
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours remaining to
overhaul/HSI/GBl:
Left Engine P27094 8140 10755 3330/923/2723
Right Engine P20322 3718 4975 1693/1073/2873
2.2.3 Propeller Type Number: Serial Number: Overhaul Due Date:
Left Propeller HC-B3TN-5E BVA 6125 2014-12-16
Right Propeller HC-B3TN-5E BVA 6718 2015-11-15
2.2.4 Avionics System: Type / Part Number: Note:
Autopilot & Flight Director Century IV
COM/NAV/GPS 1 Garmin GNS 530
COM/NAV/GPS 2 Garmin GNS 430
Audiopanel Bendix/King KMA-24H-70
MKR Bendix/King KR-21
DME Bendix/King KDM-706
ADF Bendix/King KDF-806
XPDR 1 Garmin GTX 330D Mode S EHS
XPDR 2 Garmin GTX 330 *) Mode S EHS
RDR ALT Bendix/King KRA-10A
ELT Kanad ELT 406-AF-H
Airspeed Indicator LH / RH Aerosonic 20040-161 / 20040-
0186
Altimeter LH United Instr. Inc. 5934 PAD-1
Altimeter incl. encoder RH United Instr. Inc. 5035P-P40
Altitude Reporter Narco AR 850
Altitude Alerter Aero Mechanism AM 275C
Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3
Attitude Gyro & Flight Director Ind. Century 52C77
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LH
Attitude Gyro Ind. RH AIM 504-0006-914
Turn & Bank Ind. LH R.C Allen A5930-02
Horizontal Situation Indicator LH Bendix/King KPI-553A
DG-Gyro Sperry C-14A
Directional Gyro RMI Ind. LH AIM 254-1D
CDI Indicator Garmin GI-106A
*) XPDR 2 without diversity configuration
2.2.5 Mission System System: Description:
Fixed general installations
VHF/UHF COM 1 & 2 FR31
GPS MAP
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
Laser Prism
MIL-STD-1553 Bus LH Wing Pylon
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ASTOR Fixed installed system
ADRIAN Pod mounted system LH and RH Wing
Pylon
U95 N Pod mounted system LH Wing Pylon
A100 Pod mounted system LH Wing Pylon
Missile Threat Simulator
DARTS Pod mounted system LH Wing Pylon
Chaff Dispenser
BOX 3 Pod mounted system LH and RH Wing
Pylon
2.2.6 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, U95-N, A100,
DARTS and BOX 3 General Signal Harness AWG22 shielded x 44
General Signal Harness AWG22 shielded x 50
U95-N and A100 MIL-STD-1553B Data
Bus
Triax Cable x 1
U95-N, A100 and DARTS AC Power
115/200VAC 400 Hz 3-
Phase 3 x 10 A
AWG 12 x 4
twisted
AWG 16 x 2
AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200
A
DC Power 28 VDC 200
A
AWG 2 x 2
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Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable
2.2.7 Antenna Layout
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2.2.8 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date
Aircraft SE-GHA
Vingstudie MU-2 AMP 2011-09-19 10470,92 11500
100 Hour Inspection AMP 2012-09-14 10568,72 10670,92 2013-09-14
200 Hour Inspection AMP 2012-09-14 10568,72 10768,72 2013-10-04
600 Hour Inspection AMP 2011-04-13 10424,42 11024,42 2014-04-12
1000 Hour Inspection AMP 2011-09-19 10470,92 11500
1200 Hour Inspection AMP 2012-09-25 10568,72 11768,72
1800 Hour Inspection AMP 2005-02-04 9700 11500
2000 Hour Inspection AMP 2005-02-03 9500 11500
1 Year Inspection AMP 2012-09-18 10568,72 2013-10-04
2 Year Inspection AMP 2012-09-20 10568,72 2014-10-04
10 Year Inspection AMP 2005-02-04 9700 2015-02-02
Engine S/N P-20322 Remaining
Engine Assembly (Overhaul) AMP 12280,1 1693,72
Engine Hot Section Inspection AMP 11660,1 1073,72
Engine Gearbox Inspection AMP 13460,1 2873,72
Engine S/N P-27094
Engine Assembly (Overhaul) AMP 13916,9 3330,52
Engine Hot Section Inspection AMP 11509,8 923,42
Engine Gearbox Inspection AMP 13309,8 2723,42
Propeller L/H O/H AMP 2009-12-17 13394,52 2014-12-16
Propeller R/H O/H AMP 2010-11-16 13382,5 2015-11-15
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2.2.9 Implemented Changes Abbreviations:
Abbr. Issued by Explanation
AAK Learjet Aircraft Accessory Kit
AD EASA, FAA, Finnish CA,
JCAB
Airwortness Directive
AMK Learjet Aircraft Mod Kit
AW Learjet Accessory Wire
LVA LFV Luftvärdighetsanvisning
LVD LFV Luftvärdighetsdirektiv
MSB Mitsubishi Mitsubishi. SB
MSR Mitsubishi Mitsubishi SR
SA Hartzell Service advisory
SB Keith, Learjet, Nyge,
Century, Garrett, MAI,
Hartzell, Mitsubishi,
Narco
Service Bullentin
SI Hartzell Service information
SIB EASA Service information bullentin
SIL Rockwell Service information letter
SL Mitsubishi Service Letter
SN Mitsubishi Service news
SR Mitsubishi Service recomendation
SSB Nyge and Garmin Sofware SB
SSK Learjet Special Spares Kit
STC Avcon, Flight Int., Keith, Supplement Type Certificate
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Mitsubishi
TDM Nyge Tekniskt Direktiv Materiel
TVO Nyge Teknisk Verkstad Order
Status date November 23rd
2012. SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Compliance Status Remarks
CENTURY, Century Flight
Systems Inc.
CENTURY SB CSB-2005-01
Check for frayed Bridle Cable 21-feb-05 16-nov-10
EASA, European Aviation Safety Agency
EASA AD 2006-0265
Incorrect transponder altitude 30-aug-06 27-nov-09
EASA AD 2009-0251-E
Portable Fire Extinguishers-Ident/Repl
25-nov-09 07-May-2010
N/A by current P/N installed
EASA AD 2009-0262
Halon 1211 Fire Extinguishers Id/Repl
EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-2010
N/A by current P/N installed
EASA AD 2009-0278
Halon 1211 Fire Extinguishers Id/Repl
EASA AD 2009-0262 22-dec-09 07-May-2010
N/A by current P/N installed
EASA AD 2010-0003
R1 Mode S Transponder -Check/Modification
11-jan-10 R1 10-mar-10 N/A due to model
EASA AD 2012-0037
KIDDE GRAVINER HAND OPERATTED FIRE EXTINGUISHER
04-Oct-2012
EASA SIB 2008-
58R1
Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN
SSB0845 Rev IR
17-dec-08 21-sep-10 N/A by SSB 0845 incorporated
EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model
FAA, U.S, Federal Aviation Administration
FAA, U.S AD 2000-09-15 FAA, U.S AD
2000-02-25
1 Flight in Icing Condition AFM De-icing
FINNISH AD M 2435/97 FINNISH AD M 2786/00 MAI SB 086/74-002 Rev A MAI
SB 093/22-009 MAI SB 096/30-004
07-jul-00 1 22-nov-01 Action not required due to s/n. N/A Due to paragraph b.
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MITSUBISHI SB 226 Rev E MITSUBISHI SB
231 Rev B MITSUBISHI SB 232 Rev A
FAA, U.S AD 2003-
17-04
Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB
087/56-001 Rev B MITSUBISHI SB 224 Rev C
01-Oct-
2003
16-nov-10
FAA, U.S AD 2003-22-07
1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D
16-apr-04 1 17-May-2004
inserted in AFM limitations
FAA, U.S AD 2005-14-12
Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 14-sep-05 Propellerbolts previously checked u/a
FAA, U.S AD 2005-18-20
Prop de-icer "FASTprop" 14-Oct-2005
12-Oct-2005
N/A Due to boots p/n
FAA, U.S AD 2006-13-15
Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 241 Rev A
11-aug-06 18-mar-03 c/o in conjunction with vingstudie
FAA, U.S AD 2006-15-07
Safety evaluation (feathering linkage)
MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229
FAA, U.S AD 2006-17-01
Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 Rev B
22-sep-06 21-sep-06 PCW see MSB 233A
FAA, U.S AD 2006-
17-05
Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 16-nov-10
FAA, U.S AD 2007-
17-09
Reduce max deflect elev nose-down
trim
MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's.
FAA, U.S AD 71-
14-01
Fuel Tank Fungus Coating Peeling 01-May-1972 01-jan-96 N/A by s/n
FAA, U.S AD 74-
11-01
Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
30-jan-78 05-May-
1974
FAA, U.S AD 75-
16-13
Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev
A MITSUBISHI SB 167 Rev D
05-aug-75 18-jan-77 Revision C PCW by Swedair.
FAA, U.S AD 75-16-20
Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 MITSUBISHI SB 168 Rev A
12-aug-75 20-jan-88
FAA, U.S AD 78-03-05
Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB
180 Rev A
23-feb-78 18-jan-88
FAA, U.S AD 81-
06-01
1 Engine Aft Nacelles 01-apr-81 1 22-nov-97 Previously complied with
FAA, U.S AD 81-
25-04
1 Engine's Electrical wiring SB 036/71-
003A, SB 043/71-005
21-jan-82 1 02-dec-10 N/A N/A by model
FAA, U.S AD 82-
08-02
Electrical Wiring Inspection 15-apr-82 18-mar-82
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FAA, U.S AD 83-
08-01
2 To preclude prop. attach bolt
failures
FINNISH AD M 1168/83 Rev 1 FINNISH AD
T5114/05 HARTZELL SI 140A Rev 9
28-apr-82 2 20-May-
2005
Ref. MU2B MM chap 13.4 when using bolts P/N B-
3339 only
FAA US AD 83-09-
02
Strobe Light Assemblies 16-Mar-
2012
FAA, U.S AD 84-
12-04
Torque of Air Tube Coupling Nuts SB
047/30-001, SB 196A
MAI SB 047/30-001 Rev A MITSUBISHI SB
196 Rev A
28-jun-84 31-jul-84
FAA, U.S AD 84-25-02
Elevator TrimTab Bracket Insp/Repl. SB 031/27-005 R1, SB 176E
MAI SB 031/27-005 Rev 1 MITSUBISHI SB 176 Rev E
18-dec-84 18-apr-85
FAA, U.S AD 86-
15-03
NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2
Rev B
13-aug-86 15-jul-04 Found SB 181 part 2 PCW.
FAA, U.S AD 86-
20-01
To assure anti-ice capability of pitot
SB
LFV LVD2015 Rev B 06-Oct-
1986
07-feb-00
FAA, U.S AD 86-
26-02
To prevent engine flameout in an
iceing SB 74-0003, SR 040/74-001
GARRETT SB 74-0003 Rev 6 MAI SR
040/74-001 MITSUBISHI SB 226 Rev E
MITSUBISHI SR 066
31-dec-87 09-mar-09 see applicable engine for c/o
FAA, U.S AD 87-
04-03
Addit. Seal and Flap Flexible Shaft
Insp SB 051/27-007, SB 198
MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 14-jun-85
FAA, U.S AD 87-12-02
Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 17-May-1990
FAA, U.S AD 88-13-01
Bendix Autopilot Disengagement SB 066/22-006
LFV LVD2190 MAI SB 066/22-006 Rev A MITSUBISHI SB 206
11-jul-98 06-jun-89 N/A N/A due to Autopilot model
FAA, U.S AD 88-21-01
1 To minimize confusion in autopilot/manua SB 066/22-006
LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-2012
FAA, U.S AD 88-
23-01
To prevent flap control failure SB
067/27-008, SB 189B
LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 15-feb-95
FAA, U.S AD 93-
07-11
ELECTRIC TRIM SYSTEM SB 079/27-
010
LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n
FAA, U.S AD 94-
04-16
Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 31-mar-93
FAA, U.S AD 94-
11-04
Change of Flight Idle Blade Angel SB
016/61-001
LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n
FAA, U.S AD 96-
25-02
Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-
4552-96 LFV LVD2749
27-dec-96 13-feb-02
FAA, U.S AD 97-
04-13
Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-
1997
N/A N/A due to s/n.
FAA, U.S AD 97-
20-14 CNL
Icing related incidents/accidents 17-Oct-
1997
02-dec-98
FAA, U.S AD 97-
25-02
To prevent loss of airplane
ctrl/overspe
FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17
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FAA, U.S AD 98-
20-39
Forward fitting bolt of wingtip tank
SB
LFV LVD2688 19-Oct-
1998
29-nov-96
FINNISH, Finnish Civil
Aviation Adm.
FINNISH AD M
1177/83
Kontroll av rören till strobe-kablarna MITSUBISHI SB 174 PART 1 Rev C 07-jul-83 16-nov-10
FINNISH AD M
2609/98
Justering av br,nslefl"de MHI SB
097/73-001, TCD-4890-98
JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 16-nov-10
FINNISH AD M
3076
Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 21-aug-03 16-nov-10
GARMIN, Garmin
GARMIN SSB 0844 Software Version 5.04 EASA SIB2008-58R1 19-May-
2010
A 14-nov-08
GARMIN SSB
0845
Software Version 6.04 EASA SIB2008-58R1 19-May-
2010
O 14-nov-08
GARRETT, AlliedSignal
Aerospace
GARRETT SB 74-
0003
6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 6 09-mar-09 see applicable engine for c/o
HARTZELL,
Hartzell Propeller
Inc.
HARTZELL SB 61-256
Propeller mounting bolt inspection MITSUBISHI SL 053/72-003 , MITSUBISHI SL 080
08-feb-02 06-jun-02
HARTZELL SB 61-279 ALERT
4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL 085
04-Oct-2005
4 14-nov-05 Propellerbolts previously checked u/a
HARTZELL SB A61-313
3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , FAA, U.S AD 2009-10-14
15-jul-09 3 21-sep-10 N/A by SSB 0845 incorporated
HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 Rev A
30-mar-05 9 13-mar-08 see previously revision
JCAB, Japan Civil Aviation
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Bureau
JCAB AD TCD-0642-70
JCAB AD TCD-0518-68
AFM revision regarding fuel spec.
Rivet holes elevator hinge fitting
LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 18-jan-88
JCAB AD TCD-
0643-70
Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-Jul-2004
26-Mar-2009
N/A N/A by s/n. by s/n
JCAB AD TCD-0652-70
Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-0653-70
Engine Nacelle Tail Area-Modification of
25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-0660-70
Replacement of bearing in nosegearstrut
LFV LVA457 MITSUBISHI SB 123 01-May-1970
26-mar-09 N/A by s/n
JCAB AD TCD-
0730-1-72
Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev
B
25-mar-72 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
0730-2-86
Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n
JCAB AD TCD-
0859-72
Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 09-Oct-
1972
N/A N/A due to s/n.
JCAB AD TCD-
0866-72
NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-
1972
31-dec-72 N/A N/A due to s/n.
JCAB AD TCD-
0947A-74
Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev
A
12-nov-74 18-jan-88 N/A N/A due to s/n.
JCAB AD TCD-0948A-1-78
Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09
JCAB AD TCD-0948A-74
Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev B
07-Oct-1974
05-May-1974
JCAB AD TCD-1001A-76
Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev E
06-Oct-1976
18-apr-85
JCAB AD TCD-1001B-2-84
Replacement of Elevator Trim Tab Bracket
FINNISH AD M 1080/82 LFV LVD1971 MITSUBISHI SB 176 Rev E
12-dec-84 18-apr-85
JCAB AD TCD-1094A-76
Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A MITSUBISHI SB 167 Rev D
06-sep-76 18-jan-77 Revision C PCW by Swedair.
JCAB AD TCD-1188-75
Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 MITSUBISHI SB 168 Rev A
06-May-1975
20-jan-88
JCAB AD TCD-1202-75
Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW.
JCAB AD TCD-1209-75
Insp/mod of NLG shimmydamper locking
LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 10-jul-75
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2012-12-06
Document number Page
60(195)
JCAB AD TCD-
1235-75
Insp./repl. of MLG fwd door
emerg.cables
LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 18-jan-88 N/A N/A due to model.
JCAB AD TCD-
1272-75
Supp.,MLG Forward D. Actuating
Mech.-I&M
MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model
JCAB AD TCD-
1284-1-76
Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173
JCAB AD TCD-1328-76
Fire hazard in rear baggage compartment
01-jul-76 26-mar-09 N/A by s/n
JCAB AD TCD-
1353-76
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by s/n
JCAB AD TCD-
1370-76
Inspect strobelight conduit in
Tiptank
LFV LVA1196 18-Oct-
1976
18-jan-88 Part.1
JCAB AD TCD-
1370A-81
Inspect strobelight conduit in
Tiptank supersed TCD-1370-76
MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 16-nov-10
JCAB AD TCD-
1379-1-80
Insp. rear eng. cowling reg.
heatdamage
LFV LVA1197 Rev A MITSUBISHI SB 177
Rev B
06-feb-02 22-nov-77 Previously complied with
JCAB AD TCD-
1520A-77
Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180
JCAB AD TCD-
1768-1-85
Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.
JCAB AD TCD-
1817-79
Modification of
bagagecompartment
LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
JCAB AD TCD-
2048-81
Insp. firewarning & emerg.power
circuit
LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-
1985
N/A N/A due to s/n.
JCAB AD TCD-
2070-81
Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 12-Oct-
1981
JCAB AD TCD-
2113-82
Insp./replace engine electrical
harness
LFV LVA1788 MITSUBISHI SB 191 06-feb-02 18-mar-82
JCAB AD TCD-
2252-2-88
Flap system torquetubes supersed
TCD-2252-1-87
01-feb-89 24-mar-09 PCW
JCAB AD TCD-
2252-83
Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 15-feb-95
JCAB AD TCD-
2263-83
NLG. bracket attaching to drag strut 13-aug-83 24-mar-09 N/A by model
JCAB AD TCD-2342-1-84
Engine inlet anti-ice tubing. Torq./lock
MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW
JCAB AD TCD-2342-84
Engine inlet anti-ice tubing. Torq./lock
LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 31-jul-84
JCAB AD TCD-2450A-87
Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.
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2012-12-06
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JCAB AD TCD-
2451-1-87
Add. seal/Tq. insp of flap flex. shaft 01-May-
1987
09-mar-09 PCW see TCD-2451-85
JCAB AD TCD-
2451-85
Add. seal/Tq. insp of flap flex. shaft
Superseeded by TCD-2451-1-87
LFV LVD2037 MITSUBISHI SB 198 30-sep-85 14-jun-85
JCAB AD TCD-
2545-1-88
Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 17-May-
1990
JCAB AD TCD-2679A-97
Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 MITSUBISHI SB 226 Rev E
01-feb-97 22-nov-01
JCAB AD TCD-
2856-1-97
Bendix M4C Autopilot System MITSUBISHI SB 206 05-nov-97 16-nov-09 N/A due to Autopilot model
JCAB AD TCD-
3378-90
Insp./mod. of rudder trimtab
leadingedge
LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
3393A-96
Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev
1 MITSUBISHI SB 212 Rev A
25-May-
1996
16-nov-10
JCAB AD TCD-
3464-91
Unintentional engagement of
A/P......
17-jun-91 24-mar-09 N/A by model
JCAB AD TCD-
3740A-98
Mod.of Autopilote pitchtrimsystem
MSB 216, 228 LVD 2898
FINNISH AD M 2581/98 LFV LVD2450 LFV
LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228
17-aug-98 27-Oct-
1998
JCAB AD TCD-3901-93
Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 MITSUBISHI SB 221
10-sep-93 21-feb-94
JCAB AD TCD-3942-1-94
Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 MITSUBISHI SB 219 Rev A
28-nov-94 24-mar-95
JCAB AD TCD-
3942-94
Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 08-mar-95
JCAB AD TCD-
4310-96
Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688
MITSUBISHI SB 225
01-apr-96 29-nov-96
JCAB AD TCD-
4311-95
Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678
MITSUBISHI SB 224 Rev C
01-nov-95 16-nov-10
JCAB AD TCD-
4379-96
Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689
MITSUBISHI SB 229
01-apr-96 30-jul-96
JCAB AD TCD-
4552-96
Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 13-feb-02
JCAB AD TCD-
4625-97
Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB
093/22-009
14-jul-97 04-Oct-
2001
JCAB AD TCD-
4625A-2001
Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B
NYGE TDM01-45
16-mar-01 13-mar-09 PCW Ref AMOC LFV Appr M15/01, TDM 01-45
JCAB AD TCD-
4626-97
De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800
MITSUBISHI SB 232 Rev A
01-May-
1997
14-jul-04 PCW
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2012-12-06
Document number Page
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JCAB AD TCD-
4684-97
Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819
MITSUBISHI SB 230
01-jun-97 25-mar-99
JCAB AD TCD-
4753-98
Ändring av flyghandbok LVD
2922,FAA AD 97-20-14, MHI SN 117A
FINNISH AD M 2518/98 LFV LVD2922
MITSUBISHI SN 117 Rev D
18-feb-98 02-dec-98 FAA AD utförd.
JCAB AD TCD-4753A-2004
Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-2004
inserted in AFM limitations
JCAB AD TCD-
4838-98
Inspection of landing gear power
train
FINNISH AD M 2574/98 LFV LVD2897
MITSUBISHI SB 235
04-aug-98 24-mar-09 N/A by model
JCAB AD TCD-
4889-2-2007
Inappropriate calib. of eng. trq-
meter
MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.
JCAB AD TCD-
4889-98
Insp. of Engine Torque Indication
System LFV 2924, MU SB 233
FINNISH AD M 2608/98 LFV LVD2924
MITSUBISHI SB 233 Rev B
05-nov-98 14-jul-04 PCW
JCAB AD TCD-
4890-98
Check of flight idle FF LVD 2925, MU
SB 234
FINNISH AD M 2609/98 LFV LVD2925
MITSUBISHI SB 234
04-nov-98 16-nov-10
JCAB AD TCD-
5030-99
Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-
1999
24-mar-09 N/A by model
JCAB AD TCD-5432-2000
AFM revision LFV LVD3112 27-nov-00 12-feb-02
JCAB AD TCD-5547-2001
To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02
JCAB AD TCD-5747-2001
Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 04-Oct-2001
JCAB AD TCD-
5864-2001
Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 17-jan-02
JCAB AD TCD-
6127-2003
Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 04-nov-03
JCAB AD TCD-
7030-2006
Inspection of Wing Attachment
Hardware
MITSUBISHI SB 241 Rev A 27-dec-06 17-jan-07 c/o in conjunction with wingstudie
LFV,
Luftfartsverket
LFV LVA 1011 A Kontroll av vingklaffarnas manöversystem
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 MITSUBISHI SB 167 Rev D
05-feb-02 A 18-jan-77 Revision C PCW by Swedair.
LFV LVA 1012 Kontroll av propellerreglagets montering
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 MITSUBISHI SB 168 Rev A
05-feb-02 20-jan-88
LFV LVA 1013 Kontr. och mod. av låsning på nosställ
JCAB AD TCD-1209-75 MITSUBISHI SB 169 Rev B
05-feb-02 10-jul-75
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2012-12-06
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LFV LVA 1014 A Kontr. & byte av motorinkl.
låsanordning
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
05-feb-02 A 18-jan-88
LFV LVA 1083 Insp. & utbyte av lina för nödöppning
JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A
05-feb-02 18-jan-88 N/A N/A due to s/n.
LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174 PART 1 Rev C
06-feb-02 16-nov-10
LFV LVA 1197 A Förhindr. av värmeskador på
bak.motorpl.
JCAB AD TCD-1379-1-80 MITSUBISHI SB
177 Rev B
06-feb-02 A 22-nov-77 Previously complied with
LFV LVA 1238 Kontr. & byte av infästningsdet.
trimrod
06-feb-02 21-apr-09 N/A by s/n
LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-
1-85 MITSUBISHI SB 181 PART 2 Rev B
06-feb-02 18-jan-88
LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
LFV LVA 1740 Kontr.av brandvarnings-och
n"dstr"mskret
JCAB AD TCD-2048-81 MITSUBISHI SB 187
Rev B
05-feb-02 31-aug-09 N/A by s/n
LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 12-Oct-
1981
LFV LVA 1788 Kontroll/Utbyte av elledningar på
motor
JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 18-mar-82
LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB 189
Rev C
06-feb-02 15-feb-95
LFV LVA 1942 Momentdragning/låsn.av koppl.i varmlufts
JCAB AD TCD-2342-84 MITSUBISHI SB 196 Rev A
06-feb-02 31-jul-84
LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 15-jul-04 N/A N/A by s/n.
LFV LVA 439 Rev. av flyghandbok betr.
bränslespec.
JCAB AD TCD-0642-70 MITSUBISHI SB 112
Rev C
05-feb-02 18-jan-88
LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model
LFV LVA 457 Utbyte av lager i nosst,llets
st"td,mp.
JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n
LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.
LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 16-nov-09 N/A by s/n
LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n
LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB 162 Rev A
05-feb-02 A 18-jan-88 N/A N/A due to s/n.
LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03- 05-feb-02 A 05-May-
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2012-12-06
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06 JCAB AD TCD-0948A-74 MITSUBISHI SB
163 Rev B
1974
LFV LVA 886 A Kontroll/byte av
höjdtrimroderarmar
JCAB AD TCD-1001A-76 05-feb-02 A 18-apr-85
LFV LVD 1238 Kontr./byte infästn.det.
höjdtrimroder
15-apr-77 31-aug-09 N/A by s/n
LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB 176 Rev E
18-jan-85 18-apr-85
LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-
005 Rev A, MHI SR 53
FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 MAI SR 020/34-005
MITSUBISHI SR 053A
24-May-
1985
B 06-mar-86
LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 14-jun-85
LFV LVD 2069 Altimeter 25-mar-86 18-jan-88 N/A N/A by p/n & s/n
LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA
26-jan-87 11-sep-87
LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006 och SB 206
FAA, U.S AD 88-13-01 MAI SB 066/22-006 Rev A MITSUBISHI SB 206
19-aug-88 17-May-1990
N/A Bendix A/P ej installerad
LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB 201 Rev A
19-aug-88 25-Oct-1988
LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-
1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C
08-dec-88 15-feb-95
LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-dec-88 12-feb-02
LFV LVD 2338 Kont./Mod.av sidorodrets
trimroderframka Mitsubishi MHI SB
211
JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
LFV LVD 2347 1 Control Deice-system Mitsubishi SB
212A
JCAB AD TCD-3393A-96 MITSUBISHI SB
212 Rev A
29-May-
1996
1 16-nov-10
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13
CHPT 9
23-May-
1991
05-jun-91 checked OK.
LFV LVD 2450 Elevator Trim Tab Installation MU SB
216
JCAB AD TCD-3740A-98 MITSUBISHI SB
216
03-dec-92 31-mar-93
LFV LVD 2477 Electric Trim System AD930711, MU
SB 079/27-0-010
FAA, U.S AD 93-07-11 MAI SB 079/27-010 03-jun-93 27-mar-09 N/A by s/n
LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 21-feb-94
LFV LVD 2537 Reducering av Höjdrodrets trimområde. FAA AD 94-04-16, SB
FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 31-mar-93
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2012-12-06
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216
LFV LVD 2538 Byte Låspinne i landställets nödutf.
SB 219
JCAB AD TCD-3942-94 MITSUBISHI SB 219
Rev A
07-apr-94 24-mar-95
LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n
LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox TCD-3942-1-94, MSB 219A
JCAB AD TCD-3942-1-94 MITSUBISHI SB 219 Rev A
09-feb-95 24-mar-95
LFV LVD 2678 Kontr. av vindrutor och fönster MHI
SB 224 Rev A
FAA, U.S AD 2003-17-04 JCAB AD TCD-
4311-95 MITSUBISHI SB 224 Rev C
12-mar-96 16-nov-10
LFV LVD 2688 Kontr/byte av infästn.bult för
tiptank MU-2 SB 225
FAA, U.S AD 98-20-39 JCAB AD TCD-4310-
96 MITSUBISHI SB 225
09-May-
1996
29-nov-96
LFV LVD 2689 Kontroll av linkage för prop.flöjning
MU-2 SB 229
JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-
1996
30-jul-96
LFV LVD 2732 Inspection/ Replacement of Prop
Hub. FAA AD 96-18-14, Hz SB 136H
FAA, U.S AD 96-18-14 HARTZELL SB 61-
261 Rev 1
27-sep-96 09-mar-98 Prop. utbytt mot BVA
LFV LVD 2749 Revision av flyghandbok AFM TCD-
4552-96
FAA, U.S AD 96-25-02 JCAB AD TCD-4552-
96
21-jan-97 13-feb-02
LFV LVD 2761 Installation av autoignition system
TCD-2679A-97
JCAB AD TCD-2679A-97 MITSUBISHI SB
226 Rev E
14-feb-97 19-mar-99
LFV LVD 2769 Demont.av backventil i bränslesystemets MU-2 SB 130A
FAA, U.S AD 97-04-13 MITSUBISHI SB 130 Rev A
18-mar-97 05-May-1997
N/A due to s/n.
LFV LVD 2800 Mod. av De-ice Monitoring System Mitsubishi SB 232, TCD-4626-97
JCAB AD TCD-4626-97 MITSUBISHI SB 232 Rev A
28-aug-97 08-May-1998
LFV LVD 2819 Mod.av lagerboxar för landställssystem Mitsubishi SB 230
JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 09-mar-98
LFV LVD 2853 Periodisk funktionskontroll av nödutgång
23-mar-98 16-nov-10
LFV LVD 2897 Kontroll av landst,llets drivsystem TCD-4838-98, SB 235
JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model
LFV LVD 2898 Mod. av autopilotens höjdtrimsystem TCD-3740A-98, SB 216, 228
JCAB AD TCD-3740A-98 MITSUBISHI SB 216 MITSUBISHI SB 228
27-aug-98 27-Oct-1998
LFV LVD 2922 Änd.av Flyghandbok-Extra krav på typutbi TCD-4753-98, MHI SN 117A
JCAB AD TCD-4753-98 MITSUBISHI SN 117 Rev D
12-nov-98 02-dec-98 FAA AD utförd.
LFV LVD 2924 Kontr/Just av motorernas Torque indikeri MHI SB 233, TCD-4889-98
JCAB AD TCD-4889-98 MITSUBISHI SB 233 Rev B
01-dec-98 19-mar-99
LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id MHI SB 234
JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 08-apr-10
LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209 18-jun-99 24-mar-09 N/A by model
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Rev B
LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02
LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-009 MITSUBISHI SB 231 Rev B NYGE TDM01-45
02-apr-01 04-Oct-2001
Ref AMOC LFV Appr M15/01, TDM 01-45
LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02
LFV LVD 3166 Sprickkontroll av infästning till ving-
spetstank
JCAB AD TCD-5747-2001 MITSUBISHI SB
236
20-sep-01 04-Oct-
2001
LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-
012 MITSUBISHI SB 237
09-jan-02 17-jan-02
LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB
239
21-mar-03 04-nov-03
MAI, Mitsubishi Aircraft
International
MAI SB 047/30-001
A Torque of Bleed Air Tube Coupling Nuts AD 84-12-04,SB 196A
FAA, U.S AD 84-12-04 MITSUBISHI SB 196 Rev A
19-jul-84 A 31-jul-84
MAI SB 051/27-007
Add.Seal and Flap Flexible Shaft Torque AD 87-04-03, SB 198
FAA, U.S AD 87-04-03 01-feb-85 14-jun-85
MAI SB 067/27-008
A Insp/Repl. of Flap Control System Torque AD 88-23-01, SB 189B
FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 15-feb-95
MAI SB 069/24-006
Split Radio Bus Inspection and Rework
MAI SB 066/22-006 Rev A 17-nov-88 06-jun-89 N/A N/A due to Aircraft s/n
MAI SB 086/74-002
A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2435/97 MITSUBISHI SB 226 Rev E
05-Oct-2000
A 22-nov-01 Action not required due to s/n.
MAI SB 089/57-
002
A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 29-nov-96 N/A N/A due to s/n.
MAI SN 110/00-
017A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MAI SN 111/77-
004
Torque Indicating System Shift
Potential
20-nov-08 11-mar-09 SB 233 considered
MAI SR 020/34-
005
Anti Ice Capability AD 86-20-01, SR
053A
FAA, U.S AD 86-20-01 LFV LVD2015 Rev B
MITSUBISHI SR 053A
06-Oct-
1986
07-feb-00 N/A N/A due to s/n.
MITSUBISHI, Mitsubishi Heavy Industries Ltd
MITSUBISHI MSR B **RECOVERED RECORD** 11-sep-87
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
67(195)
066
MITSUBISHI SB
066
Bendix M4D 18-dec-87 17-May-
1990
N/A
MITSUBISHI SB
076/22-008
M-4() Autop.Engage Switch Guard
Install.
11-apr-91 12-apr-95 N/A
MITSUBISHI SB
112
C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-
1971
C 18-jan-88
MITSUBISHI SB
114
Fuel Quantity Indicator
Readjustmnet
JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.
MITSUBISHI SB
119
The Bolt and Bolt Hole Diam. of
Nose L.G
JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model
MITSUBISHI SB 123
Bearing,Oleo Strut,Nose L.G. -Repl. of
JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n
MITSUBISHI SB 124
Scissors Switch,Nose L.G. -Install. of 31-aug-70 18-jan-88 N/A
MITSUBISHI SB 128
B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n
MITSUBISHI SB 143
B Top Coating, Wing Integral Main F.T.-SIo
JCAB AD TCD-0730-1-72 JCAB AD TCD-0730-2-86
05-jan-72 B 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 162
A Flex. Shafts, Flap Control Sys.-Insp. of (AD750201)
JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-1974
A 18-jan-88 N/A
MITSUBISHI SB 163
B Insp. of Outer Pane, Front Winds. & Inst
FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A
16-nov-78 05-May-1974
MITSUBISHI SB 165
A Lubr. Interval,Wheel Bearing,Main & Nose
24-jul-80 19-jan-88 N/A
MITSUBISHI SB 166
Wing Flap 24-jul-80 18-jan-88 N/A
MITSUBISHI SB 167
D Flap M.Jack Screw-Insp. of and/or Main G
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 LFV LVA1011 Rev A
24-jul-80 D 18-jan-77 Revision C PCW by Swedair.
MITSUBISHI SB 168
A Propeller Pitch Control Lever-Insp. of (AD761620)
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 LFV LVA1012
24-jul-80 A 20-jan-88
MITSUBISHI SB 169
B Shimmy Damper-Insp. and Modification of
JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW
MITSUBISHI SB 170
A MLG Forward Door Em.Op. Cable-Insp. & Re (AD762204)
JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 18-jan-88 N/A N/A due to s/n
MITSUBISHI SB 171
B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 LFV LVA1014 Rev A
17-nov-77 B 18-jan-88
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
68(195)
MITSUBISHI SB
173
A Drag Strut, Main L.G.-Modification
of
JCAB AD TCD-1284-1-76 24-jul-80 12-feb-76
MITSUBISHI SB
174 PART 1
C Tip Tank Conduit Tube-Insp.of,and
Rew.of (AD830902)
FINNISH AD M 1177/83 JCAB AD TCD-
1370A-81 LFV LVA1196
02-Oct-
1981
C 16-nov-10
MITSUBISHI SB
175
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A
MITSUBISHI SB 176
E Elevator Trim Tab Bracket-Repl. of LVD1971, AD 84-25-02, SB 031/27-
005R1
FAA, U.S AD 84-25-02 FINNISH AD M 1080/82 JCAB AD TCD-1001A-76 JCAB AD
TCD-1001B-2-84 LFV LVD1971
26-sep-84 E 18-apr-85
MITSUBISHI SB
177
B Mod. of Engine Nacelle Tail Area
(AD810601)
JCAB AD TCD-1379-1-80 LFV LVA1197 Rev
A
11-sep-80 B 22-nov-77 Previously complied with
MITSUBISHI SB
179
Rodd Assem., Engine Nacelle Upper
D.-R&M
27-May-
1977
25-Oct-
1988
MITSUBISHI SB
180
A Link, Engine Nacelle Upper D.-Repl.
of (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A
17-nov-77 A 20-apr-78
MITSUBISHI SB 181 PART 2
B Insp. and Repl. of Nose L.G. Strut Assem (AD801812)
FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 LFV LVA1546
08-apr-85 B 18-jan-88
MITSUBISHI SB
182
Add. of Ceiling Cover, Rear Bagg.
Comp.
JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n.
MITSUBISHI SB
184
Turnbuckle, Control Cables -Repl. of 04-apr-80 05-feb-88
MITSUBISHI SB
188
Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 12-Oct-
1981
MITSUBISHI SB
189
C Flap Control Torque Tube AD 88-23-
01, SB 067/27-008
FINNISH AD M 2722/00 JCAB AD TCD-
2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202
28-jun-94 C 15-feb-95
MITSUBISHI SB 190
A Trav. Nut Repl. of L.G. Mech. Stop Assem
28-jun-94 06-dec-83
MITSUBISHI SB
191
Engine El. Wire-Insp. and
Replacement of (AD820802)
JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 18-mar-82
MITSUBISHI SB
193
B Landing Gear Warning Horn
Syst.Modif.
15-jun-94 B 04-dec-00 Rev A är utförd.
MITSUBISHI SB
194
Master Cauting Light Visibility-Impr.
of
23-aug-82 23-mar-83
MITSUBISHI SB
196
A Ret. of coupling nut on the bleed air
tu AD 84-12-04, SB 047/30-001
FAA, U.S AD 84-12-04 JCAB AD TCD-2342-
1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A
12-apr-84 A 31-jul-84
MITSUBISHI SB 198
Add. Seal & Torque Insp. of Flap Flex.Sh LVD2037, AD 87-04-03, SB
FAA, U.S AD 87-04-03 JCAB AD TCD-2451-85 LFV LVD2037
13-feb-85 14-jun-85
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
69(195)
051/27-007
MITSUBISHI SB
199
A Engine Lubricating Tubing Insp. &
Protec
24-jun-94 A 06-nov-09 PCW
MITSUBISHI SB
200
B Insp of Nose Ldg Gear Drag Strut
Link
24-jun-94 A 25-Oct-
1988
MITSUBISHI SB
201
A Generator Circuit Wires Insp. and
Mod.
FAA, U.S AD 87-12-02 JCAB AD TCD-2545-
1-88 LFV LVD2191
02-mar-88 A 17-May-
1990
MITSUBISHI SB
204
Speed Placard Change 03-mar-87 05-feb-88
MITSUBISHI SB
206
Bendix Autop.Disengagement
Method Stand.
FAA, U.S AD 88-13-01 JCAB AD TCD-2856-
1-97 LFV LVD2190
13-Oct-
1987
31-jan-89 N/A N/A due to Autopilot model
MITSUBISHI SB 207
Rudder T.T. & Elevator T.T. Insp. & Rep.
20-May-1988
27-nov-09
MITSUBISHI SB 209
B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model
MITSUBISHI SB 210
A Engine Ignition Unit Replacement 12-nov-96 06-mar-98
MITSUBISHI SB 211
Rudder Trim Tab Modification (LVD 2338)
JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A
MITSUBISHI SB 212
A Insp of Anti-ice/Deice Systems (LVD 2347),
JCAB AD TCD-3393A-96 LFV LVD2347 Rev 1
25-apr-96 A 16-nov-10
MITSUBISHI SB 214
Engine Control Rod Inspection 06-dec-91 31-mar-93
MITSUBISHI SB 215
Removel of Prop. Governor Speed Signal
23-Oct-1991
31-jan-92 N/A N/A due to -1 engine
MITSUBISHI SB 216
Elevator Trim Tab Installation (LVD 2450
FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV LVD2450 LFV LVD2537 LFV LVD2898
11-sep-92 31-mar-93
MITSUBISHI SB 218
A Propeller Feathering Linkage Inspection
17-jan-94 A 21-feb-94
MITSUBISHI SB 219
A Emergency Gear Down G.box Lower Pin Repl
JCAB AD TCD-3942-1-94 JCAB AD TCD-3942-94 LFV LVD2538 LFV LVD2592
24-Oct-1994
A 24-mar-95
MITSUBISHI SB 221
Tip Tank Conduit Tube Insp. and Rep.
JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 21-feb-94
MITSUBISHI SB 222
Fuselage Waterproof Modification SR 019
28-jun-94 19-mar-99
MITSUBISHI SB 223
Pitot/Static System Improvement SR 064
MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 07-feb-00
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
70(195)
MITSUBISHI SB
224
C Acrylic Windsheild/Window glass
Insp. UHB
FAA, U.S AD 2003-17-04 FINNISH AD M
3076 JCAB AD TCD-4311-95 LFV LVD2678
30-apr-98 C 16-nov-10
MITSUBISHI SB
225
Forward fitting bult of wingtip tank
LVD 2688
FAA, U.S AD 98-20-39 FINNISH AD M
2351/96 JCAB AD TCD-4310-96 LFV LVD2688
29-sep-95 29-nov-96
MITSUBISHI SB 226
E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97
FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD-
2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A
18-sep-01 E 22-nov-01 PCW
MITSUBISHI SB 227
Rudder Torque Tube Modification 20-dec-96 09-mar-98
MITSUBISHI SB 228
Elevator Trim Indicator Modification LFV 2898
FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898
13-jul-98 27-Oct-1998
MITSUBISHI SB 229
Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689
20-feb-96 30-jul-96
MITSUBISHI SB 230
Mod.of Bearing Box Ldg. Gear Act. LVD 2819
JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 09-mar-98
MITSUBISHI SB 231
B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV
LVD3122 MAI SB 093/22-009 NYGE
TDM01-45
11-dec-02 B 03-mar-03 SL 079 allready performed.
MITSUBISHI SB 232
A De-Ice System Modification LVD 2800, TCD-4626-97
FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2786/00 JCAB AD TCD-4626-97 LFV
LVD2800 MAI SB 096/30-004
06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev 0.
MITSUBISHI SB
233
B Insp.of Engine Torque Indication
System. TCD-4889-98, LFV 2924
FAA, U.S AD 2006-17-01 FINNISH AD M
2608/98 JCAB AD TCD-4889-2-2007 JCAB
AD TCD-4889-98 LFV LVD2924
08-mar-07 B 18-apr-07 Checked, previously carried out
MITSUBISHI SB
234
Fl.Check of the Flight Idle Fuel Flow
Se TCD-4890-98, LVD 2925
FAA, U.S AD 2006-17-05 JCAB AD TCD-
4890-98 LFV LVD2925
07-Oct-
1998
16-nov-10
MITSUBISHI SB
235
Inspection of landing gear power
train
JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model
MITSUBISHI SB
236
Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 04-Oct-
2001
MITSUBISHI SB
237
Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02
MITSUBISHI SB 238
Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
71(195)
MITSUBISHI SB
239
Pneumatic Line Insp. and
Modification
JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 04-nov-03
MITSUBISHI SB
240
Inst.of Trottle Quadrant Placard 26-feb-03 20-Oct-
2003
MITSUBISHI SB
241
A Inspection of Wing Attachment
Hardware
FAA, U.S AD 2006-13-15 JCAB AD TCD-
7030-2006
21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie
MITSUBISHI SL 060
System 17-feb-89 28-jun-91
MITSUBISHI SL
078
Automatic Autopilot Disconnect
System
28-jan-02 16-nov-10
MITSUBISHI SL
079
Diode inst.in Flap Position
Ind.Curcuit
28-jan-02 04-Oct-
2001
MITSUBISHI SL
080
Hartzell Propeller Mounting Bolt
Insp.
HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.
MITSUBISHI SL
084
Pneumatic De-Ice Monitoring
System
14-jun-04 16-nov-10
MITSUBISHI SL
085
Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-
2005
14-sep-05 Propellerbolts previously checked u/a
MITSUBISHI SN
053
B Rudder Torque Tube AD 86-20-01,
SB 020/34-005
05-nov-86 B 17-jan-88
MITSUBISHI SN
117
D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD
TCD-4753-98 LFV LVD2922
14-jun-04 D 17-May-
2004
MITSUBISHI SN
146
Water Ingress into Vertical Stabilizer 19-dec-03 12-mar-04
MITSUBISHI SN
148
Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB
MITSUBISHI SN
156A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MITSUBISHI SN
157
Torque Indicating System Shift
Potential
20-nov-08 11-mar-09 SB 233 considered
MITSUBISHI SN
161
Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE
MITSUBISHI SN
164
IR Part 2, one time inspection of
mechanical stop bearing.
04-Oct-
2012
MITSUBISHI SR 053A
Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-2450A-87 LFV LVD2015 Rev B MAI SR
020/34-005 MITSUBISHI SB 223
23-Oct-1984
06-mar-86
MITSUBISHI SR
064
Pitot & Static System MITSUBISHI SB 223 30-apr-85 27-feb-00
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
72(195)
MITSUBISHI SR
065
Warning Horn 20-jan-86 18-jan-88
MITSUBISHI SR
067
Emergency Exit Placard 17-sep-85 18-jan-88
MITSUBISHI SR
072
Air Filter Replacement for Vacuum
Syst.
25-apr-00 09-dec-05
MITSUBISHI SR 075
Inst. tip tank placard 29-Oct-2004
01-jun-05
MITSUBISHI STC
SA01913SE
Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-09 11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection
NARCO, Narco
NARCO SB ELT10-
16
ELT ASSY 18-apr-88 28-jun-91 N/A
NYGE, Saab Aerotech Aircraft Services
NYGE TDM 01-45 Installation of Trim-In-Motion Alert
Syst. and Automatic A/P Disconnect syst.
JCAB AD TCD-4625A-2001 LFV LVD3122
MITSUBISHI SB 231 Rev B
07-May-
2001
04-Oct-
2001
NYGE TDM 02-10 Installation of TPE331-6-252M Engines
25-mar-02 04-Oct-2001
NYGE TDM 02-24 Installation Moving MAP 10-Oct-2002
28-Oct-2002
NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04
NYGE TDM 02-33 Viktminskning MU-2B 24-dec-02 01-mar-04
NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 install.
04-mar-03 8 31-Oct-2008
NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 06-Oct-2003
Original compliance was as per TDM rev A.The A/C installation is IAW rev C as not affected by rev B
and C.F01322, F01347, F01349
NYGE TDM 03-15 A U95 with General Control System 24-apr-03 A 25-feb-08
NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 27-nov-09 Original compliance by Rev D. Not affected by rev
F.
NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05
NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 01-Oct-
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
73(195)
2007
NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06 A 07-feb-08
NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07 A 07-feb-08
NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 28-feb-08
NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 27-nov-09
NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 31-Oct-
2008
Original compliance with TDM rev A. Rev B does
not affect previous complaiance.
NYGE TDM 09-22 A Electrical Wiring Feed Through 08-sep-09 A 27-nov-09
NYGE TDM 09-27 A GPS Splitter 12-Oct-
2009
A 27-nov-09
NYGE TDM 09-33 A MU-2B Loudspeaker in Cockpit 04-dec-09 A 04-May-
2010
C/W
NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 19-May-2010
C/W
NYGE TDM 10-46 A MU-2 Alternate lap top computers A 10-Jun-2011
NYGE TDM 11-35 A Terminating resistor A 27-Jan-2012
NYGE TDM 12-21 A Avinstallation IK 14-Aug-2012
NYGE TDM 12-40 A MU-2B Relocation of MIC/Phone Jacks
04-Oct-2012
NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 18-mar-03
NYGE TDM 97-03 Astor MU-2 25-feb-97 04-mar-98
NYGE TDM 98-08 Torrluft ASTOR 27-May-
1998
17-aug-98
NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 19-mar-99
NYGE TVO 1/09 Inspektion av Stringers & struktur
vinge
25-feb-09 04-mar-09 Inspected with remarks
NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 31-mar-93
NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 09-Oct-
1998
NYGE TVO 1/97 3 De-Icertank MU-2B,
korrosionskontroll
12-feb-97 13-feb-97
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
74(195)
NYGE TVO 2/00 Märkning av infästning domkraft
Mu2
01-dec-00 15-nov-00
NYGE TVO 2/07 A Prevent FR31 radio to xmit when
RM2 off
06-feb-07 A 28-feb-07
NYGE TVO 2/91 A/C Elecrical System 10-jan-91 07-aug-91
NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06 16-nov-10
NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 27-nov-09
NYGE TVO 4/11 A Static Inverter controll 15-Dec-2011
NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 16-nov-10
NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 07-aug-91
NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 12-jun-92
NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 07-apr-10
NYGE TVO 4/96 Kontroll av Lagerhus i
noshjulsstyrning.
25-Oct-
1996
11-May-
1997
Utförd tidigare (ref.Ove N lista)
NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 07-apr-10
NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-
1992
12-nov-92
NYGE TVO 7/93 Starter Drive Splines 01-nov-93 18-jan-96
NYGE TVO 8/04 Kontr. av Spant vid bakre
feninfästning
08-dec-04 07-apr-10
NYGE TVO 8/92 Wheel Parts 27-Oct-
1992
31-mar-93
NYGE TVO 9/88 Emergency Extension System 08-aug-88 25-Oct-
1988
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
75(195)
2.3 GFE Aircraft Mitsubishi MU-2 SE-GHB
2.3.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
MU-2B-20 287 SE-GHB 11585 6415 2012-11-23
2.3.2 Engines Type: Honeywell TPE331-6-252M
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours remaining to
Overhau/HSI/GBI:
Left Engine P20019 11797 11513 1916/197/116
Right Engine P20146 9513 13195 3142/1346/1342
2.3.3 Propeller Type Number: Serial Number: Overhaul Due Date:
Left Propeller HC-B3TN-5C BVA 6205 2013-09-14
Right Propeller HC-B3TN-5E BVA 6253 2013-03-26
2.3.4 Avionics System: Type / Part Number: Note:
Autopilot & Flight Director Century IV
COM/NAV/GPS 1 Garmin GNS 530
COM/NAV/GPS 2 Garmin GNS 430
Audiopanel Bendix/King KMA-24H-70
MKR Bendix/King KR-21
DME Bendix/King KDM-706
ADF Bendix/King KDF-806
XPDR 1 Garmin GTX 330D Mode S EHS
XPDR 2 Garmin GTX 330 *) Mode S EHS
RDR ALT Bendix/King KRA-10A
ELT Kanad ELT 406-AF-H
Airspeed Indicator LH / RH Aerosonic 065A-986402-003 /
20040-161
Altimeter LH United Instr. Inc. 5934 PAD-1
Altimeter incl. encoder RH United Instr. Inc. 5035P-P40
Altitude Reporter Narco AR 850
Altitude Alerter Aero Mechanism AM 275C
Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
76(195)
Attitude Gyro & Flight Director Ind.
LH
Century 52C77
Attitude Gyro Ind. RH AIM 504-0006-914
Turn & Bank Ind. LH R.C Allen A5930-02
Horizontal Situation Indicator LH Bendix/King KPI-553A
DG-Gyro Sperry C-14A
Directional Gyro RMI Ind. LH AIM 254-1D
CDI Indicator Garmin GI-106A
*) XPDR 2 without diversity configuration
2.3.5 Mission System System: Description:
Fixed general installations
VHF/UHF COM 1 & 2 FR31
GPS MAP
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
Laser Prism
MIL-STD-1553 Bus LH Wing Pylon
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ASTOR Fixed installed system
ADRIAN Pod mounted system LH and RH Wing
Pylon
U95 N Pod mounted system LH Wing Pylon
U95 Sorc Pod mounted system RH Wing Pylon
A100 Pod mounted system LH Wing Pylon
Missile Threat Simulator
DARTS Pod mounted system LH Wing Pylon
Chaff Dispenser
BOX 3 Pod mounted system LH and RH Wing
Pylon
Precisions GPS Pos System
TAPS
2.3.6 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, U95-N, A100,
DARTS and BOX 3 General Signal Harness AWG22 shielded x 44
General Signal Harness AWG22 shielded x 50
U95-N and A100 MIL-STD-1553B Data
Bus
Triax Cable x 1
U95-N, A100 and DARTS AC Power
115/200VAC 400 Hz 3-
AWG 12 x 4
twisted
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
77(195)
Phase 3 x 10 A AWG 16 x 2
AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200
A
DC Power 28 VDC 200
A
AWG 2 x 2
Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable
2.3.7 Antenna Layout
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
78(195)
2.3.8 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date
Aircraft SE-GHB
Vingstudie MU-2 AMP 2012-02-23 11477 12500
100 Hour Inspection AMP 2012-03-01 11477 11577,4 2013-03-01
200 Hour Inspection AMP 2012-03-14 11477 11677,4 2013-05-18
600 Hour Inspection AMP 2011-03-08 11412 12012 2014-04-17
1000 Hour Inspection AMP 2012-03-27 11477 12500
1200 Hour Inspection AMP 2007-07-31 11047 12247,5
1800 Hour Inspection AMP 2007-07-31 11047 12847,5
2000 Hour Inspection AMP 2012-03-22 11477 13500
1 Year Inspection AMP 2012-05-15 11477,4 2013-05-18
2 Year Inspection AMP 2012-01-23 11457,2 2014-01-22
10 Year Inspection AMP 2005-02-24 10500 2015-02-22
Engine S/N P-20019 Remaining
Engine Assembly (Overhaul) AMP 13501,9 1916,85
Engine Hot Section Inspection AMP 11782,8 197,75
Engine Gearbox Inspection AMP 11702 116,95
Engine S/N P-20146
Engine Assembly (Overhaul) AMP 14727,2 3142,15
Engine Hot Section Inspection AMP 12931,8 1346,75
Engine Gearbox Inspection AMP 12927,2 1342,15
Propeller L/H O/H AMP 2008-09-15 14211,1 2013-09-14
Propeller R/H O/H AMP 2008-03-27 14144 2013-03-26
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
79(195)
2.3.9 Implemented Changes Status dateNovember 23
rd 2012.
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Complianc
e
Stat
us
Remarks
CENTURY, Century Flight
Systems Inc.
CENTURY SB CSB-2005-01
Check for frayed Bridle Cable 21-feb-05 31-mar-10
EASA, European Aviation
Safety Agency
EASA AD 2006-0265
Incorrect transponder altitude 30-aug-06 14-jan-10
EASA AD 2009-0251-E
Portable Fire Extinguishers-Ident/Repl 25-nov-09 07-May-2010
N/A N/A by current P/N installed
EASA AD 2009-
0262
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-
0278
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2010-
0003
R1 Mode S Transponder -
Check/Modification
11-jan-10 R1 10-mar-10 N/A due to model
EASA AD 2012-
0037
KIDDE GRAVINER HAND OPERATTED
FIRE EXTINGUISHER
06-Sep-
2012
EASA SIB 2008-
58R1
Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN
SSB0845 Rev IR
17-dec-08 21-sep-10 N/A by SSB 0845 incorporated
EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model
FAA, U.S, Federal Aviation Administration
FAA, U.S AD 2000-02-25
AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b.
FAA, U.S AD 2000-
09-15 FAA, U.S AD
1 Flight in Icing Condition AFM De-icing FINNISH AD M 2435/97 FINNISH AD M
2786/00 MAI SB 086/74-002 Rev A MAI SB
07-jul-00 02-apr-02 N/A Due to paragraph b.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
80(195)
2000-02-25 093/22-009 MAI SB 096/30-004
MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A
FAA, U.S AD 2003-22-07
1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D
16-apr-04 17-May-2004
inserted in AFM limitations
FAA, U.S AD 2005-14-12
Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 14-sep-05
FAA, U.S AD 2005-18-20
Prop de-icer "FASTprop" 14-Oct-2005
12-Oct-2005
N/A Due to boots p/n
FAA, U.S AD 2006-13-15
Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 241 Rev A
11-aug-06 17-nov-03 c/o in conjunction with vingstudie
FAA, U.S AD 2006-15-07
Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229
FAA, U.S AD 2006-17-01
Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 Rev B
22-sep-06 21-sep-06 PCW see MSB 233A
FAA, U.S AD 2006-17-05
Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 27-sep-10
FAA, U.S AD 2007-
17-09
Reduce max deflect elev nose-down
trim
MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's.
FAA, U.S AD 71-
14-01
Fuel Tank Fungus Coating Peeling 01-May-
1972
01-jan-96 N/A by s/n
FAA, U.S AD 74-
11-01
Windshield Outer Panes COP
2011/09/1 19:37:04
LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
30-jan-78 16-May-
1974
FAA, U.S AD 75-
16-13
Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev
A MITSUBISHI SB 167 Rev D
05-aug-75 25-mar-77 Revision C PCW by Swedair.
FAA, U.S AD 75-
16-20
Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012
MITSUBISHI SB 168 Rev A
12-aug-75 20-May-
1975
FAA, U.S AD 78-03-05
Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB
180 Rev A
23-feb-78 25-nov-75
FAA, U.S AD 81-
06-01
1 Engine Aft Nacelles 01-apr-81 1 25-May-
1997
Previously complied with
FAA, U.S AD 81-
25-04
1 Engine's Electrical wiring SB 036/71-
003A, SB 043/71-005
21-jan-82 1 02-dec-10 N/A N/A by model
FAA, U.S AD 82-
08-02
Electrical Wiring Inspection 15-apr-82 09-feb-82
FAA, U.S AD 83-
08-01
2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD
T5114/05 HARTZELL SI 140A Rev 9
28-apr-82 2 20-May-
2005
Ref. MU2B MM chap 13.4 when using bolts P/N
B-3339 only
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
81(195)
FAA US AD 83-09-
02
Strobe light assembles 16-Mar-12
FAA, U.S AD 84-
12-04
Torque of Air Tube Coupling Nuts SB
047/30-001, SB 196A
MAI SB 047/30-001 Rev A MITSUBISHI SB
196 Rev A
28-jun-84 16-feb-84
FAA, U.S AD 84-
25-02
Elevator TrimTab Bracket Insp/Repl.
SB 031/27-005 R1, SB 176E
MAI SB 031/27-005 Rev 1 MITSUBISHI SB
176 Rev E
18-dec-84 23-apr-85
FAA, U.S AD 86-15-03
NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 Rev B
13-aug-86 15-jul-04 Found SB 181 part 2 PCW.
FAA, U.S AD 86-
20-01
To assure anti-ice capability of pitot
SB 020/34-005, SB 053A
LFV LVD2015 Rev B MAI SR 020/34-005
MITSUBISHI SR 053A
06-Oct-
1986
30-aug-00
FAA, U.S AD 86-
26-02
To prevent engine flameout in an
iceing SB 74-0003, SR 040/74-001
GARRETT SB 74-0003 Rev 6 31-dec-87 09-mar-09 see applicable engine for c/o
FAA, U.S AD 87-
04-03
Addit. Seal and Flap Flexible Shaft
Insp SB 051/27-007, SB 198
MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 29-jul-85
FAA, U.S AD 87-
12-02
Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 23-apr-90
FAA, U.S AD 88-
13-01
Bendix Autopilot Disengagement SB
066/22-006
LFV LVD2190 MAI SB 066/22-006 Rev A
MITSUBISHI SB 206
11-jul-98 22-dec-89 N/A N/A due to Autopilot model
FAA, U.S AD 88-
21-01
1 To minimize confusion in
autopilot/manua SB 066/22-006
LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-12
FAA, U.S AD 88-
23-01
To prevent flap control failure SB
067/27-008, SB 189B
LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 18-May-
1995
FAA, U.S AD 93-
07-11
ELECTRIC TRIM SYSTEM SB 079/27-
010
LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n
FAA, U.S AD 94-
04-16
Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 12-Oct-
1993
FAA, U.S AD 94-
11-04
Change of Flight Idle Blade Angel SB
016/61-001
LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n
FAA, U.S AD 96-
25-02
Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-
4552-96 LFV LVD2749
27-dec-96 12-nov-97
FAA, U.S AD 97-
04-13
Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-
1997
N/A N/A due to s/n.
FAA, U.S AD 97-
20-14 CNL
Icing related incidents/accidents 17-Oct-
1997
02-dec-98
FAA, U.S AD 97-25-02
To prevent loss of airplane ctrl/overspe
FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17
FAA, U.S AD 98-20-39
Forward fitting bolt of wingtip tank SB MU-2 225, 089/57-002A
LFV LVD2688 MAI SB 089/57-002 Rev A MITSUBISHI SB 225
19-Oct-1998
07-Oct-1997
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
82(195)
FAIRCHILD,
Fairchild Aircraft
FAIRCHILD SB 29-
005
2 In Service Hydraulic Leaks FAA, U.S AD 85-04-01 Rev 1 19-Jul-1985 02-jan-00 23-apr-85
FINNISH, Finnish Civil
Aviation Adm.
FINNISH AD M
2461/97
Avisningens "vervakningsanl,ggning JCAB AD TCD-4626-97 01-aug-97 11-mar-10
FINNISH AD M
2609/98
Justering av br,nslefl"de MHI SB
097/73-001, TCD-4890-98
JCAB AD TCD-4890-98, MAI SB 097/73-
001
12-nov-99 27-sep-10
GARMIN, Garmin
GARMIN SSB
0844
IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 20-May-
2010
GARMIN SSB
0845
IR Software Version 6.04 EASA SIB2008-58R1 14-nov-08 0 20-May-
2010
GARRETT,
AlliedSignal
Aerospace
GARRETT SB 74-0003
6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 09-mar-09 see applicable engine for c/o
HARTZELL,
Hartzell Propeller
Inc.
HARTZELL SB 61-
256
Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI
SL 080
08-feb-02 02-Oct-
2002
HARTZELL SB 61-279 ALERT
4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 04-Oct-2005
14-nov-05 Propellerbolts previously checked u/a
HARTZELL SB A61-313
3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , FAA, U.S AD 2009-10-14
15-jul-09 3 20-sep-10 N/A by SSB 0844
HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2, LFV LVA1424 Rev A
30-mar-05 9 13-mar-08 see previously revision
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
83(195)
JCAB, Japan Civil Aviation
Bureau
JCAB AD TCD-
0518-68
Rivet holes elevator hinge fitting 06-Feb-
1968
26-mar-09 N/A by s/n
JCAB AD TCD-
0642-70
AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 30-jun-89
JCAB AD TCD-0643-70
Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A by s/n
JCAB AD TCD-
0652-70
Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-
0653-70
Engine Nacelle Tail Area-Modification
of
25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-
0660-70
Replacement of bearing in
nosegearstrut
LFV LVA457 MITSUBISHI SB 123 01-May-
1970
26-mar-09 N/A by s/n
JCAB AD TCD-
0730-1-72
Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev
B
25-mar-72 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
0730-2-86
Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n
JCAB AD TCD-
0859-72
Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to s/n.
JCAB AD TCD-
0866-72
NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-
1972
31-dec-72 N/A N/A due to s/n.
JCAB AD TCD-
0947A-74
Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev
A
12-nov-74 16-May-
1974
N/A N/A due to s/n.
JCAB AD TCD-
0948A-1-78
Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09
JCAB AD TCD-
0948A-74
Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
07-Oct-
1974
16-May-
1974
JCAB AD TCD-
1001A-76
Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev
E
06-Oct-
1976
23-apr-85
JCAB AD TCD-
1001B-2-84
Replacement of Elevator Trim Tab
Bracket
FINNISH AD M 1080/82 LFV LVD1971
MITSUBISHI SB 176 Rev E
12-dec-84 23-apr-85
JCAB AD TCD-
1094A-76
Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A
MITSUBISHI SB 167 Rev D
06-sep-76 25-mar-77 Revision C PCW by Swedair.
JCAB AD TCD-1188-75
Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 MITSUBISHI SB 168 Rev A
06-May-1975
20-May-1975
JCAB AD TCD-1202-75
Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB
180 Rev A
20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
84(195)
JCAB AD TCD-
1209-75
Insp/mod of NLG shimmydamper
locking
LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 16-jun-75
JCAB AD TCD-
1235-75
Insp./repl. of MLG fwd door
emerg.cables
LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 30-jun-89 N/A N/A due to model.
JCAB AD TCD-
1272-75
Supp.,MLG Forward D. Actuating
Mech.-I&M
MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model
JCAB AD TCD-1284-1-76
Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173
JCAB AD TCD-
1328-76
Fire hazard in rear baggage
compartment
01-jul-76 26-mar-09 N/A by s/n
JCAB AD TCD-
1353-76
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by s/n
JCAB AD TCD-
1370-76
Inspect strobelight conduit in Tiptank LFV LVA1196 18-Oct-
1976
22-dec-89 Part.1
JCAB AD TCD-
1379-1-80
Insp. rear eng. cowling reg.
heatdamage
LFV LVA1197 Rev A MITSUBISHI SB 177
Rev B
06-feb-02 25-May-
1977
Previously complied with
JCAB AD TCD-
1520A-77
Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180
JCAB AD TCD-
1768-1-85
Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 2
Rev B
12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.
JCAB AD TCD-
1817-79
Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
JCAB AD TCD-
2048-81
Insp. firewarning & emerg.power
circuit
LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-
1981
N/A N/A due to s/n.
JCAB AD TCD-
2070-81
Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 02-sep-81
JCAB AD TCD-
2113-82
Insp./replace engine electrical
harness
LFV LVA1788 MITSUBISHI SB 191 06-feb-02 09-feb-82
JCAB AD TCD-
2252-2-88
Flap system torquetubes supersed
TCD-2252-1-87
01-feb-89 24-mar-09 PCW
JCAB AD TCD-
2252-83
Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 18-May-
1995
JCAB AD TCD-
2263-83
NLG. bracket attaching to drag strut 13-aug-83 24-mar-09 N/A by model
JCAB AD TCD-2342-1-84
Engine inlet anti-ice tubing. Torq./lock
MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW
JCAB AD TCD-2342-84
Engine inlet anti-ice tubing. Torq./lock
LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 16-feb-84
JCAB AD TCD-2450A-87
Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
85(195)
JCAB AD TCD-
2451-1-87
Add. seal/Tq. insp of flap flex. shaft 01-May-
1987
09-mar-09 PCW see TCD-2451-85
JCAB AD TCD-
2451-85
Add. seal/Tq. insp of flap flex. shaft
Superseeded by TCD-2451-1-87
LFV LVD2037 MITSUBISHI SB 198 30-sep-85 29-jul-85
JCAB AD TCD-
2545-1-88
Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 23-apr-90
JCAB AD TCD-2679A-97
Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 MITSUBISHI SB 226 Rev E
01-feb-97 22-nov-01
JCAB AD TCD-
3378-90
Insp./mod. of rudder trimtab
leadingedge
LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s7n.
JCAB AD TCD-
3393A-96
Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev
1 MITSUBISHI SB 212 Rev A
25-May-
1996
31-May-
2010
JCAB AD TCD-
3464-91
Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model
JCAB AD TCD-
3740A-98
Mod.of Autopilote pitchtrimsystem
MSB 216, 228 LVD 2898
FINNISH AD M 2581/98 LFV LVD2450 LFV
LVD2898 MITSUBISHI SB 216 MITSUBISHI
SB 228
17-aug-98 25-mar-99
JCAB AD TCD-3901-93
Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 MITSUBISHI SB 221
10-sep-93 01-mar-94
JCAB AD TCD-3942-1-94
Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 MITSUBISHI SB 219 Rev A
28-nov-94 08-mar-95
JCAB AD TCD-3942-94
Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 08-mar-95
JCAB AD TCD-
4310-96
Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688
MITSUBISHI SB 225
01-apr-96 07-Oct-
1997
JCAB AD TCD-
4379-96
Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689
MITSUBISHI SB 229
01-apr-96 30-jul-96
JCAB AD TCD-
4552-96
Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 12-feb-02
JCAB AD TCD-
4625-97
Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB
093/22-009
14-jul-97 02-apr-02
JCAB AD TCD-
4625A-2001
Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16-mar-01 02-apr-02 PCW Ref AMOC LFV Appr M15/01, TDM 01-45
JCAB AD TCD-
4626-97
De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800
MITSUBISHI SB 232 Rev A
01-May-
1997
14-jul-04 PCW
JCAB AD TCD-
4684-97
Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819
MITSUBISHI SB 230
01-jun-97 25-mar-99
JCAB AD TCD-
4753-98
Ändring av flyghandbok LVD
2922,FAA AD 97-20-14, MHI SN 117A
FINNISH AD M 2518/98 LFV LVD2922
MITSUBISHI SN 117 Rev D
18-feb-98 02-dec-98 FAA AD utförd.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
86(195)
JCAB AD TCD-
4753A-2004
Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-
2004
inserted in AFM limitations
JCAB AD TCD-
4838-98
Inspection of landing gear power
train
FINNISH AD M 2574/98 LFV LVD2897
MITSUBISHI SB 235
04-aug-98 24-mar-09 N/A by model
JCAB AD TCD-
4889-2-2007
Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.
JCAB AD TCD-4889-98
Insp. of Engine Torque Indication System LFV 2924, MU SB 233
FINNISH AD M 2608/98 LFV LVD2924 MITSUBISHI SB 233 Rev B
05-nov-98 14-jul-04 PCW
JCAB AD TCD-
4890-98
Check of flight idle FF LVD 2925, MU
SB 234
FINNISH AD M 2609/98 LFV LVD2925
MITSUBISHI SB 234
04-nov-98 27-sep-10
JCAB AD TCD-
5030-99
Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-
1999
24-mar-09 N/A by model
JCAB AD TCD-
5432-2000
AFM revision LFV LVD3112 27-nov-00 12-feb-02
JCAB AD TCD-
5547-2001
To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02
JCAB AD TCD-
5747-2001
Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 11-Oct-
2001
JCAB AD TCD-
5864-2001
Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 16-May-
2002
JCAB AD TCD-
6127-2003
Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 14-nov-03
JCAB AD TCD-
7030-2006
Inspection of Wing Attachment
Hardware
MITSUBISHI SB 241 Rev A 27-dec-06 17-jan-07 c/o in conjunction with wingstudie
LFV,
Luftfartsverket
LFV LVA 1011 A Kontroll av vingklaffarnas manöversystem
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 MITSUBISHI SB 167 Rev D
05-feb-02 A 25-mar-77 Revision C PCW by Swedair.
LFV LVA 1012 Kontroll av propellerreglagets
montering
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-
75 MITSUBISHI SB 168 Rev A
05-feb-02 20-May-
1975
LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169
Rev B
05-feb-02 16-jun-75
LFV LVA 1014 A Kontr. & byte av motorinkl.
låsanordning
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
05-feb-02 A 25-nov-75
LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A
05-feb-02 30-jun-89 N/A N/A due to s/n.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
87(195)
LFV LVA 1197 A Förhindr. av värmeskador på
bak.motorpl.
JCAB AD TCD-1379-1-80 MITSUBISHI SB
177 Rev B
06-feb-02 A 25-May-
1977
Previously complied with
LFV LVA 1238 Kontr. & byte av infästningsdet.
trimrod
06-feb-02 21-apr-09 N/A by s/n
LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-
1-85 MITSUBISHI SB 181 PART 2 Rev B
06-feb-02 15-mar-84
LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
LFV LVA 1740 Kontr.av brandvarnings-och
n"dstr"mskret
JCAB AD TCD-2048-81 MITSUBISHI SB 187
Rev B
05-feb-02 31-aug-09 N/A by s/n
LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 02-sep-81
LFV LVA 1788 Kontroll/Utbyte av elledningar på
motor COP 2011/09/1 19:37:04
JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 09-feb-82
LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB 189
Rev C
06-feb-02 18-May-
1995
LFV LVA 1942 Momentdragning/låsn.av koppl.i
varmlufts
JCAB AD TCD-2342-84 MITSUBISHI SB 196
Rev A
06-feb-02 16-feb-84
LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 15-jul-04 N/A N/A by s/n.
LFV LVA 439 Rev. av flyghandbok betr.
bränslespec.
JCAB AD TCD-0642-70 MITSUBISHI SB 112
Rev C
05-feb-02 30-jun-89
LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model
LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n
LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.
LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 08-dec-09 N/A by A/C serial number
LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n
LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB
162 Rev A
05-feb-02 A 16-May-
1974
N/A N/A due to s/n.
LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-
06 JCAB AD TCD-0948A-74 MITSUBISHI SB
163 Rev B
05-feb-02 A 26-mar-09
LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 23-apr-85
LFV LVD 1238 Kontr./byte infästn.det.
höjdtrimroder
15-apr-77 31-aug-09 N/A by s/n
LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB
176 Rev E
18-jan-85 23-apr-85
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
88(195)
LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005
Rev A, MHI SR 53
FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87
24-May-
1985
B 20-May-
1986
LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 29-jul-85
LFV LVD 2069 Altimeter 25-mar-86 22-dec-89 N/A N/A by p/n & s/n
LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA
26-jan-87 15-jan-88
LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006
och SB 206
FAA, U.S AD 88-13-01 MAI SB 066/22-006
Rev A MITSUBISHI SB 206
19-aug-88 22-dec-89 N/A Bendix A/P ej installerad
LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB
201 Rev A
19-aug-88 28-sep-89
LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-
1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C
08-dec-88 18-May-
1995
LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-Dec-1988 12-feb-02
LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB
211
JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
LFV LVD 2347 1 Control Deice-system Mitsubishi SB
212A
JCAB AD TCD-3393A-96 MITSUBISHI SB
212 Rev A
29-May-
1996
1 31-May-
2010
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13
CHPT 9
23-May-
1991
10-jun-91 checked OK.
LFV LVD 2450 Elevator Trim Tab Installation MU SB
216
JCAB AD TCD-3740A-98 MITSUBISHI SB
216
03-dec-92 12-Oct-
1993
LFV LVD 2477 Electric Trim System AD930711, MU
SB 079/27-0-010
FAA, U.S AD 93-07-11 MAI SB 079/27-010 03-jun-93 27-mar-09 N/A by s/n
LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 01-mar-94
LFV LVD 2537 Reducering av Höjdrodrets trimområde. FAA AD 94-04-16, SB
216
FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 12-Oct-1993
LFV LVD 2538 Byte Låspinne i landställets nödutf. SB
219
JCAB AD TCD-3942-94 MITSUBISHI SB 219
Rev A
07-apr-94 08-mar-95
LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n
LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox
TCD-3942-1-94, MSB 219A
JCAB AD TCD-3942-1-94 MITSUBISHI SB
219 Rev A
09-feb-95 08-mar-95
LFV LVD 2688 Kontr/byte av infästn.bult för tiptank
MU-2 SB 225
FAA, U.S AD 98-20-39 JCAB AD TCD-4310-
96 MITSUBISHI SB 225
09-May-
1996
07-Oct-
1997
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
89(195)
LFV LVD 2689 Kontroll av linkage för prop.flöjning
MU-2 SB 229
JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-
1996
30-jul-96
LFV LVD 2732 Inspection/ Replacement of Prop
Hub. FAA AD 96-18-14, Hz SB 136H
FAA, U.S AD 96-18-14 HARTZELL SB 61-
261 Rev 1
27-sep-96 16-May-
2002
Prop. BU10873 utbytt samt mod. till BUA
LFV LVD 2749 Revision av flyghandbok AFM TCD-
4552-96
FAA, U.S AD 96-25-02 JCAB AD TCD-4552-
96
21-jan-97 12-feb-02
LFV LVD 2761 Installation av autoignition system TCD-2679A-97
JCAB AD TCD-2679A-97 MITSUBISHI SB 226 Rev E
14-feb-97 26-mar-99
LFV LVD 2769 Demont.av backventil i
bränslesystemets MU-2 SB 130A
FAA, U.S AD 97-04-13 MITSUBISHI SB 130
Rev A
18-mar-97 05-May-
1997
N/A N/A due to s/n.
LFV LVD 2800 Mod. av De-ice Monitoring System
Mitsubishi SB 232, TCD-4626-97
JCAB AD TCD-4626-97 MITSUBISHI SB 232
Rev A
28-aug-97 27-May-
1998
LFV LVD 2819 Mod.av lagerboxar för
landställssystem Mitsubishi SB 230
JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 22-jan-98
LFV LVD 2853 Periodisk funktionskontroll av
nödutgång
23-mar-98 21-jan-11
LFV LVD 2897 Kontroll av landst,llets drivsystem
TCD-4838-98, SB 235
JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model
LFV LVD 2898 Mod. av autopilotens höjdtrimsystem
TCD-3740A-98, SB 216, 228
JCAB AD TCD-3740A-98 MITSUBISHI SB
216 MITSUBISHI SB 228
27-aug-98 12-mar-99
LFV LVD 2922 Änd.av Flyghandbok-Extra krav på
typutbi TCD-4753-98, MHI SN 117A
JCAB AD TCD-4753-98 MITSUBISHI SN 117
Rev D
12-nov-98 02-dec-98 FAA AD utförd.
LFV LVD 2924 Kontr/Just av motorernas Torque
indikeri MHI SB 233, TCD-4889-98
JCAB AD TCD-4889-98 MITSUBISHI SB 233
Rev B
01-dec-98 27-sep-99 SB 233A C/Out.
LFV LVD 2925 Kontr/just av mot bränsleflöde Flight
Id MHI SB 234
JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 27-sep-10
LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209
Rev B
18-jun-99 24-mar-09 N/A by model
LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02
LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-
009 MITSUBISHI SB 231 Rev B NYGE TDM01-45
02-apr-01 02-apr-02 Ref AMOC LFV Appr M15/01, TDM 01-45
LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02
LFV LVD 3166 Sprickkontroll av infästning till ving-spetstank
JCAB AD TCD-5747-2001 MITSUBISHI SB 236
20-sep-01 11-Oct-2001
LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-012 MITSUBISHI SB 237
09-jan-02 16-May-2002
LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB 21-mar-03 14-nov-03
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
90(195)
239
MAI, Mitsubishi Aircraft
Internation
MAI SB 047/30-001
A Torque of Bleed Air Tube Coupling Nuts AD 84-12-04,SB 196A
FAA, U.S AD 84-12-04 MITSUBISHI SB 196 Rev A
19-jul-84 A 16-feb-84
MAI SB 051/27-
007
Add.Seal and Flap Flexible Shaft
Torque AD 87-04-03, SB 198
FAA, U.S AD 87-04-03 01-feb-85 29-jul-85
MAI SB 067/27-
008
A Insp/Repl. of Flap Control System
Torque AD 88-23-01, SB 189B
FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 18-May-
1995
MAI SB 069/24-
006
Split Radio Bus Inspection and
Rework
MAI SB 066/22-006 Rev A 17-nov-88 22-dec-89 N/A N/A due to Aircraft s/n
MAI SB 089/57-
002
A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 07-Oct-
1997
N/A N/A due to s/n.
MAI SN 110/00-
017A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MAI SN 111/77-
004
Torque Indicating System Shift
Potential
20-nov-08 11-mar-09 SB 233 considered
MAI SR 020/34-005
Anti Ice Capability AD 86-20-01, SR 053A
FAA, U.S AD 86-20-01 LFV LVD2015 Rev B MITSUBISHI SR 053A
06-Oct-1986
30-aug-00 N/A N/A due to s/n.
MITSUBISHI, Mitsubishi Heavy Industries Ltd
MITSUBISHI MSR
066 B
**RECOVERED RECORD** B 15-jan-88
MITSUBISHI SB
066
Bendix M4D 18-dec-87 28-sep-89
MITSUBISHI SB
076/22-008
M-4() Autop.Engage Switch Guard Install. 11-apr-91 12-apr-95 N/A
MITSUBISHI SB
112
C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-
1971
C 30-jun-89
MITSUBISHI SB 114
Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.
MITSUBISHI SB 119
The Bolt and Bolt Hole Diam. of Nose L.G JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model
MITSUBISHI SB 123
Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n
MITSUBISHI SB Scissors Switch,Nose L.G. -Install. of 31-aug-70 30-jun-89 N/A
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
91(195)
124
MITSUBISHI SB
128
B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n
MITSUBISHI SB
143
B Top Coating, Wing Integral Main F.T.-SIo JCAB AD TCD-0730-1-72 JCAB AD TCD-
0730-2-86
05-jan-72 B 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB
162
A Flex. Shafts, Flap Control Sys.-Insp. of
(AD750201)
JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-
1974
A 16-May-
1974
N/A
MITSUBISHI SB
163
B Insp. of Outer Pane, Front Winds. & Inst FAA, U.S AD 74-11-01 JCAB AD TCD-
0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A
16-nov-78 16-May-
1974
MITSUBISHI SB 165
A Lubr. Interval,Wheel Bearing,Main & Nose
24-jul-80 29-jul-74 N/A
MITSUBISHI SB
166
Wing Flap 24-jul-80 08-jan-75
MITSUBISHI SB
167
D
Flap M.Jack Screw-Insp. of and/or Main
G
FAA, U.S AD 75-16-13 JCAB AD TCD-
1094A-76 LFV LVA1011 Rev A
24-jul-80 D 25-mar-77 Revision C PCW by Swedair.
MITSUBISHI SB
168
A Propeller Pitch Control Lever-Insp. of
(AD761620)
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-
75 LFV LVA1012
24-jul-80 A 20-May-
1975
MITSUBISHI SB
169
B Shimmy Damper-Insp. and Modification
of
JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW
MITSUBISHI SB
170
A MLG Forward Door Em.Op. Cable-Insp. &
Re (AD762204)
JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 30-jun-89 N/A N/A due to s/n
MITSUBISHI SB 171
B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 LFV LVA1014 Rev A
17-nov-77 B 25-nov-78
MITSUBISHI SB 173
A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 05-mar-76
MITSUBISHI SB 174 PART 1
C Tip Tank Conduit Tube-Insp.of,and Rew.of (AD830902)
FINNISH AD M 1177/83 JCAB AD TCD-1370A-81 LFV LVA1196
02-Oct-1981
C 18-jun-10
MITSUBISHI SB 175
Barrel Nut, Inner/Outer Wing Conn.-Repl.
JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by s/n
MITSUBISHI SB 176
E Elevator Trim Tab Bracket-Repl. of LVD1971, AD 84-25-02, SB 031/27-005R1
FAA, U.S AD 84-25-02 FINNISH AD M 1080/82 JCAB AD TCD-1001A-76 JCAB AD
TCD-1001B-2-84 LFV LVD1971
26-sep-84 E 23-apr-85
MITSUBISHI SB
177
B Mod. of Engine Nacelle Tail Area
(AD810601)
JCAB AD TCD-1379-1-80 LFV LVA1197 Rev
A
11-sep-80 B 25-May-
1977
Previously complied with
MITSUBISHI SB 179
Rodd Assem., Engine Nacelle Upper D.-R&M
27-May-1977
22-dec-89
MITSUBISHI SB 180
A Link, Engine Nacelle Upper D.-Repl. of (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 JCAB AD TCD-1520A-77 LFV LVA1014
17-nov-77 A 09-May-1978
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
92(195)
Rev A
MITSUBISHI SB
181 PART 2
B Insp. and Repl. of Nose L.G. Strut Assem
(AD801812)
FAA, U.S AD 86-15-03 JCAB AD TCD-1768-
1-85 LFV LVA1546
08-apr-85 B 15-mar-84
MITSUBISHI SB
182
Add. of Ceiling Cover, Rear Bagg. Comp. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n.
MITSUBISHI SB
184
Turnbuckle, Control Cables -Repl. of 04-apr-80 15-dec-89
MITSUBISHI SB
188
Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 02-sep-81
MITSUBISHI SB
189
C Flap Control Torque Tube AD 88-23-01,
SB 067/27-008
FINNISH AD M 2722/00 JCAB AD TCD-
2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202
28-jun-94 C 18-May-
1995
MITSUBISHI SB
190
A Trav. Nut Repl. of L.G. Mech. Stop Assem 28-jun-94 17-jan-84
MITSUBISHI SB
191
Engine El. Wire-Insp. and Replacement
of (AD820802)
JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 09-feb-82
MITSUBISHI SB
193
B Landing Gear Warning Horn Syst.Modif. 15-jun-94 B 04-dec-00 Rev A är utförd.
MITSUBISHI SB
194
Master Cauting Light Visibility-Impr. of 23-aug-82 30-May-
1983
MITSUBISHI SB
196
A Ret. of coupling nut on the bleed air tu
AD 84-12-04, SB 047/30-001
FAA, U.S AD 84-12-04 JCAB AD TCD-2342-
1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A
12-apr-84 A 16-feb-84
MITSUBISHI SB
198
Add. Seal & Torque Insp. of Flap Flex.Sh
LVD2037, AD 87-04-03, SB 051/27-007
FAA, U.S AD 87-04-03 JCAB AD TCD-2451-
85 LFV LVD2037
13-feb-85 29-jul-85
MITSUBISHI SB
199
A Engine Lubricating Tubing Insp. & Protec 24-jun-94 A 06-nov-09 PCW
MITSUBISHI SB
200
B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 17-feb-88
MITSUBISHI SB
201
A Generator Circuit Wires Insp. and Mod. FAA, U.S AD 87-12-02 JCAB AD TCD-2545-
1-88 LFV LVD2191
02-mar-88 A 23-apr-90
MITSUBISHI SB
204
Speed Placard Change 03-mar-87 23-apr-90
MITSUBISHI SB
206
Bendix Autop.Disengagement Method
Stand.
FAA, U.S AD 88-13-01 JCAB AD TCD-2856-
1-97 LFV LVD2190
13-Oct-
1987
31-jan-89 N/A N/A due to Autopilot model
MITSUBISHI SB 207
Rudder T.T. & Elevator T.T. Insp. & Rep. 20-May-1988
14-jan-10
MITSUBISHI SB 209
B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
93(195)
MITSUBISHI SB
210
A Engine Ignition Unit Replacement 12-nov-96 06-mar-98
MITSUBISHI SB
211
Rudder Trim Tab Modification (LVD
2338)
JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB
212
A Insp of Anti-ice/Deice Systems (LVD
2347),
JCAB AD TCD-3393A-96 LFV LVD2347 Rev
1
25-apr-96 A 31-May-
2010
MITSUBISHI SB 214
Engine Control Rod Inspection 06-dec-91 08-apr-92
MITSUBISHI SB
215
Removel of Prop. Governor Speed Signal 23-Oct-
1991
17-feb-92 N/A N/A due to -1 engine
MITSUBISHI SB
216
Elevator Trim Tab Installation (LVD 2450 FAA, U.S AD 2007-17-09 FAA, U.S AD 94-
04-16 JCAB AD TCD-3740A-98 LFV
LVD2450 LFV LVD2537 LFV LVD2898
11-sep-92 12-Oct-
1993
MITSUBISHI SB
218
A Propeller Feathering Linkage Inspection 17-jan-94 A 01-mar-94
MITSUBISHI SB
219
A Emergency Gear Down G.box Lower Pin
Repl
JCAB AD TCD-3942-1-94 JCAB AD TCD-
3942-94 LFV LVD2538 LFV LVD2592
24-Oct-
1994
A 08-mar-95
MITSUBISHI SB 221
Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 01-mar-94
MITSUBISHI SB 222
Fuselage Waterproof Modification SR 019
28-jun-94 27-Oct-1998
MITSUBISHI SB 223
Pitot/Static System Improvement SR 064 MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 30-aug-00
MITSUBISHI SB
224
C Acrylic Windsheild/Window glass Insp.
UHB
FAA, U.S AD 2003-17-04 FINNISH AD M
3076 JCAB AD TCD-4311-95 LFV LVD2678
30-apr-98 C 18-jun-10
MITSUBISHI SB
225
Forward fitting bult of wingtip tank LVD
2688
FAA, U.S AD 98-20-39 FINNISH AD M
2351/96 JCAB AD TCD-4310-96 LFV
LVD2688
29-sep-95 07-Oct-
1997
MITSUBISHI SB 226
E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97
FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97
FINNISH AD M 2786/00 JCAB AD TCD-2679A-97 LFV LVD2761 MAI SB 086/74-
002 Rev A
18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n.
MITSUBISHI SB
227
Rudder Torque Tube Modification 20-dec-96 04-sep-97
MITSUBISHI SB 228
Elevator Trim Indicator Modification LFV 2898
FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV
LVD2898
13-jul-98 25-mar-99 Visuell kontroll utförd SB införd
MITSUBISHI SB
229
Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-
4379-96 LFV LVD2689
20-feb-96 17-apr-98
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
94(195)
MITSUBISHI SB
230
Mod.of Bearing Box Ldg. Gear Act. LVD
2819
JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 22-jan-98
MITSUBISHI SB
231
B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD
M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE
TDM01-45
11-dec-02 B 03-mar-03 SL 079 performed earlier.
MITSUBISHI SB
232
A De-Ice System Modification LVD 2800,
TCD-4626-97
FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD
M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004
06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev 0.
MITSUBISHI SB 233
B Insp.of Engine Torque Indication System. TCD-4889-98, LFV 2924
FAA, U.S AD 2006-17-01 FINNISH AD M 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924
08-mar-07 B 18-apr-07 Checked, previously carried out
MITSUBISHI SB 234
Fl.Check of the Flight Idle Fuel Flow Se TCD-4890-98, LVD 2925
FAA, U.S AD 2006-17-05 JCAB AD TCD-4890-98 LFV LVD2925
07-Oct-1998
27-sep-10
MITSUBISHI SB 235
Inspection of landing gear power train JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model
MITSUBISHI SB 236
Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 11-Oct-2001
MITSUBISHI SB 237
Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 16-May-2002
MITSUBISHI SB 238
Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.
MITSUBISHI SB 239
Pneumatic Line Insp. and Modification JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 14-nov-03
MITSUBISHI SB
240
Inst.of Trottle Quadrant Placard 26-feb-03 14-nov-03
MITSUBISHI SB
241
A Inspection of Wing Attachment
Hardware
FAA, U.S AD 2006-13-15 JCAB AD TCD-
7030-2006
21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie
MITSUBISHI SL
060
System 17-feb-89 07-jul-91
MITSUBISHI SL
078
Automatic Autopilot Disconnect System 28-jan-02 31-May-
2010
MITSUBISHI SL
079
Diode inst.in Flap Position Ind.Curcuit 28-jan-02 02-apr-02
MITSUBISHI SL 080
Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02 02-Oct-2002
MITSUBISHI SL 084
Pneumatic De-Ice Monitoring System 14-jun-04 31-May-2010
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
95(195)
MITSUBISHI SL
085
Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-
2005
14-sep-05
MITSUBISHI SN
053
B Rudder Torque Tube AD 86-20-01, SB
020/34-005
05-nov-86 B 22-dec-89
MITSUBISHI SN
117
D
Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD
TCD-4753-98 LFV LVD2922
14-jun-04 D 17-May-
2004
MITSUBISHI SN 146
Water Ingress into Vertical Stabilizer 19-dec-03 06-mar-04
MITSUBISHI SN
148
Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB
MITSUBISHI SN
156A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MITSUBISHI SN
157
Torque Indicating System Shift Potential 20-nov-08 11-mar-09 SB 233 considered
MITSUBISHI SN
161
Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10
MITSUBISHI SR
053A
Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 LFV LVD2015 Rev B MAI SR 020/34-005 MITSUBISHI SB 223
23-Oct-
1984
20-May-
1986
MITSUBISHI SR 064
Pitot & Static System MITSUBISHI SB 223 30-apr-85 30-aug-00
MITSUBISHI SR 065
Warning Horn 20-jan-86 22-dec-89
MITSUBISHI SR
067
Emergency Exit Placard 17-sep-85 03-feb-88
MITSUBISHI SR
072
Air Filter Replacement for Vacuum Syst. 25-apr-00 17-nov-03
MITSUBISHI SR
075
Inst. tip tank placard 29-Oct-
2004
24-feb-05
MITSUBISHI STC
SA01913SE
Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-09 11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection
NARCO, Narco
NARCO SB ELT10-16
ELT ASSY 18-apr-88 10-jun-91 N/A
NYGE, Saab Aerotech
Aircraft Services
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
96(195)
NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 22-dec-97
NYGE TDM 01-45 Installation of Trim-In-Motion Alert Syst.
and Automatic A/P Disconnect syst.
JCAB AD TCD-4625A-2001 LFV LVD3122
MITSUBISHI SB 231 Rev B
07-May-
2001
02-apr-02
NYGE TDM 02-10 Installation of TPE331-6-252M Engines 25-mar-02 16-May-
2002
NYGE TDM 02-24 Installation Moving MAP 10-Oct-
2002
30-Oct-
2002
NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04
NYGE TDM 02-33 Viktminskning MU-2B 24-dec-02 27-jan-04
NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 install. 04-mar-03 20-Oct-2008
NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 05-nov-03 Original compliance was as per TDM rev A.The A/C installation is IAW rev C as not affected by rev B and C.F01323, F01346, F01348
NYGE TDM 03-15 A U95 with General Control System 24-apr-03 A 25-feb-08
NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 10-jan-10 Original compliance by Rev D. Not affected by rev F.
NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05
NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 15-jun-07
NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06 A 07-feb-08
NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07 A 07-feb-08
NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 28-feb-08
NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 14-jan-10
NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 20-Oct-2008
Original compliance with TDM rev A. Rev B does not affect previous complaiance.
NYGE TDM 09-23 A Electrical Wiring Feed Through 08-sep-09 A 10-jan-10
NYGE TDM 09-28 A GPS Splitter 12-Oct-2009
A 15-jan-10
NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May-2010
C/W
NYGE TDM 11-32 A MU-2B-20/26 Alteration oil hose A 18-May-12
NYGE TDM 11-35 A Terminating resistor A 30-Jan-12
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
97(195)
NYGE TDM 12-21 A Avinstallation IK 26-Sep-
2012
NYGE TDM 12-28 A Alteration of rivet with bolt A 18-May-12
NYGE TDM 90-09 Rep. Sprickor undre vingpanel 23-aug-90 15-sep-90
NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 17-nov-03
NYGE TDM 96-06 Rep. sprickor "hinge,front spar flange" 11-nov-96 14-nov-96
NYGE TDM 97-01 TAPS 20-feb-97 01-jan-98
NYGE TDM 97-03 Astor MU-2 25-feb-97 01-sep-97
NYGE TDM 98-08 Torrluft ASTOR 27-May-
1998
17-jul-98
NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 26-mar-99
NYGE TVO 1/09 Inspektion av Stringers & struktur vinge 25-feb-09 01-apr-09 Inspected with remarks
NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 24-jun-93
NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 26-nov-99
NYGE TVO 1/97 3 De-Icertank MU-2B, korrosionskontroll 12-feb-97 04-sep-97
NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01-dec-00 08-May-2001
NYGE TVO 2/07 A Prevent FR31 radio to xmit when RM2 off
06-feb-07 A 28-feb-07
NYGE TVO 2/91 A/C Elecrical System 10-jan-91 10-jun-91
NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 14-jan-10
NYGE TVO 4/11 A Static inverter control 15-Dec-11
NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 31-May-
2010
NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 10-jun-91
NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 17-aug-92
NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 14-jan-10 L/H & R/H
NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning. 25-Oct-1996
16-dec-96 Utförd tidigare (ref. Ove N.lista)
NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 27-sep-10
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
98(195)
NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-
1992
02-feb-93
NYGE TVO 7/93 Starter Drive Splines 01-nov-93 31-aug-94
NYGE TVO 8/04 Kontr. av Spant vid bakre feninfästning 08-dec-04 14-jan-10
NYGE TVO 8/92 Wheel Parts 27-Oct-1992
08-mar-93
NYGE TVO 9/88 Emergency Extension System 08-aug-88 18-dec-89
PIPER, The New Piper
Aircraft Inc.
PIPER SB 700 A Nose Wheel Insp/Replacement FAA, U.S AD 97-07-03 12-Oct-
1981
05-May-
1997
N/A
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
99(195)
2.4 GFE Aircraft Mitsubishi MU-2 SE-GHD
2.4.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
MU-2B-20 293 SE-GHD 11316 6411 2012-11-23
2.4.2 Engines Type: Honeywell TPE331-6-252M
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours remaining to
Overhaul/HIS/GBl:
Left Engine P20038 9616 10264 4228/628/2428
Right Engine P20052 11551 11102 3444/1642/1644
2.4.3 Propeller Type Number: Serial Number: Overhaul Due Date:
Left Propeller HC-B3TN-5E BVA 6817 At overhaul 2012-11-23
Right Propeller HC-B3TN-5E BVA 7713 At overhaul 2012-11-23
2.4.4 Avionics System: Type / Part Number: Note:
Autopilot & Flight Director Century IV
COM/NAV/GPS 1 Garmin GNS 530
COM/NAV/GPS 2 Garmin GNS 430
Audiopanel Bendix/King KMA-24H-70
MKR Bendix/King KR-21
DME Bendix/King KDM-706
ADF Bendix/King KDF-806
XPDR 1 Garmin GTX 330D Mode S EHS
XPDR 2 Garmin GTX 330 *) Mode S EHS
RDR ALT Bendix/King KRA-10A
ELT Kanad ELT 406-AF-H
Airspeed Indicator LH / RH Aerosonic 065A-986402-003 /
20040-161
Altimeter LH United Instr. Inc. 5934 PAD-1
Altimeter incl. encoder RH ARC 42540-3228
Altitude Reporter Narco AR 850
Altitude Alerter Aero Mechanism AM 275C
Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
100(195)
Attitude Gyro & Flight Director Ind.
LH
Century 52C77
Attitude Gyro Ind. RH AIM 504-0006-914
Turn & Bank Ind. LH R.C Allen A5930-02
Horizontal Situation Indicator LH Bendix/King KPI-553A
DG-Gyro Sperry C-14A
Directional Gyro RMI Ind. LH AIM 254-1D
CDI Indicator Garmin GI-106A
*) XPDR 2 without diversity configuration
2.4.5 Mission System System: Description:
Fixed general installations
VHF/UHF COM 1 & 2 FR31
GPS MAP
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
Laser Prism
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ADRIAN Pod mounted system RH Wing Pylon
Target Towing
MBV7S Inboard winch
AS200 MDI (Miss Distance Indicator)
2.4.6 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S General Signal Harness AWG22 shielded x 44
General Signal Harness AWG22 shielded x 50
AC Power
115/200VAC 400 Hz 3-
Phase 3 x 10 A
AWG 16 x 4
twisted
AWG 16 x 2
AWG 20 x 2 Adrian C & S DC Power 28 VDC 200
A
AWG 2 x 2
Prepared installation Ethernet LAN Cable
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
101(195)
2.4.7 Antenna Layout
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
102(195)
2.4.8 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date
Aircraft SE-GHD
Vingstudie MU-2 AMP 2009-03-27 11158 12158,8
100 Hour Inspection AMP 2010-08-19 11260 11360 2011-08-19
200 Hour Inspection AMP 2009-12-16 11158 11358,8 2010-12-16
600 Hour Inspection AMP 2009-12-16 11158 11758,8 2012-12-15
1000 Hour Inspection AMP 2009-12-17 11158 12158,8
1200 Hour Inspection AMP 2005-05-02 10773 11973
1800 Hour Inspection AMP 2005-05-02 10773 12573
2000 Hour Inspection AMP 2004-10-14 9500 11500
1 Year Inspection AMP 2009-12-16 11158 2010-12-16
2 Year Inspection AMP 2009-12-16 11158 2011-12-16
10 Year Inspection AMP 2004-10-14 9500 2014-10-12
Engine S/N P-20038 Remaining
Engine Assembly (Overhaul) AMP 15544,9 4228,8
Engine Hot Section Inspection AMP 11944,9 628,8
Engine Gearbox Inspection AMP 13744,9 2428,8
Engine S/N P-20052
Engine Assembly (Overhaul) AMP 14760,6 3444,5
Engine Hot Section Inspection AMP 12958,8 1642,7
Engine Gearbox Inspection AMP 12960,6 1644,5
Propeller L/H O/H (not installed) AMP
Propeller R/H O/H (not installed) AMP
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
103(195)
2.4.9 Implemented Changes Status date November 23
rd 2012.
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Complianc
e
Stat
us
Remarks
CENTURY, Century Flight
Systems Inc.
CENTURY SB CSB-
2005-01
Check for frayed Bridle Cable 21-feb-05 20-aug-10
EASA, European Aviation
Safety Agency
EASA AD 2009-
0251-E
Portable Fire Extinguishers-Ident/Repl 25-nov-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-
0262
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-
0278
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2010-
0003
R1 Mode S Transponder -
Check/Modification
11-jan-10 R1 10-mar-10 N/A due to model
EASA SIB 2008-58R1
Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN SSB0845 Rev IR
17-dec-08 21-sep-10 N/A by SSB 0845 incorporated
EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model
FAA, U.S, Federal Aviation Administration
FAA, U.S AD 2000-02-25
AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b.
FAA, U.S AD 2000-
09-15
1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M
2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004
MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A
07-jul-00 1 14-jun-02
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
104(195)
FAA, U.S AD 2003-
17-04
Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB
087/56-001 Rev B MITSUBISHI SB 224 Rev C
01-Oct-
2003
20-aug-10
FAA, U.S AD 2003-22-07
1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D
16-apr-04 1 09-jun-04 Inserted in AFM Limitation Section
FAA, U.S AD 2005-14-12
Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 14-sep-05
FAA, U.S AD 2005-18-20
Prop de-icer "FASTprop" 14-Oct-2005
12-Oct-2005
N/A Due to boots p/n
FAA, U.S AD 2006-13-15
Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 241 Rev A
11-aug-06 19-jun-02 c/o in conjunction with vingstudie
FAA, U.S AD 2006-15-07
Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229
FAA, U.S AD 2006-17-01
Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 Rev B
22-sep-06 21-sep-06 PCW see MSB 233A
FAA, U.S AD 2006-17-05
Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 13-sep-10
FAA, U.S AD 2007-
17-09
Reduce max deflect elev nose-down
trim
MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's.
FAA, U.S AD 71-14-
01
Fuel Tank Fungus Coating Peeling 01-May-1972 01-jan-96 N/A N/A by s/n
FAA, U.S AD 74-11-
01
Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
30-jan-78 01-apr-76
FAA, U.S AD 75-16-
13
Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev
A MITSUBISHI SB 167 Rev D
05-aug-75 06-May-
1977
Revision C PCW by Swedair.
FAA, U.S AD 75-16-
20
Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012
MITSUBISHI SB 168 Rev A
12-aug-75 24-feb-75
FAA, U.S AD 78-03-05
Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB
180 Rev A
23-feb-78 30-dec-77
FAA, U.S AD 81-06-
01
1 Engine Aft Nacelles 01-apr-81 1 06-May-
1997
Previously complied with
FAA, U.S AD 81-25-
04
1 Engine's Electrical wiring SB 036/71-
003A, SB 043/71-005
21-jan-82 1 02-dec-10 N/A N/A by model
FAA, U.S AD 82-08-
02
Electrical Wiring Inspection 15-apr-82 15-feb-82
FAA, U.S AD 83-08-
01
2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD
T5114/05 HARTZELL SI 140A Rev 9
28-apr-82 2 20-May-
2005
Ref. MU2B MM chap 13.4 when using bolts P/N B-
3339 only
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
105(195)
FAA US AD 83-09-
02
Stobe light assemblies 16-Mar-12
FAA, U.S AD 84-12-
04
Torque of Air Tube Coupling Nuts SB
047/30-001, SB 196A
MAI SB 047/30-001 Rev A MITSUBISHI SB
196 Rev A
28-jun-84 04-jun-84
FAA, U.S AD 84-25-
02
Elevator TrimTab Bracket Insp/Repl.
SB 031/27-005 R1, SB 176E
MAI SB 031/27-005 Rev 1 MITSUBISHI SB
176 Rev E
18-dec-84 11-mar-86
FAA, U.S AD 86-15-03
NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 Rev B
13-aug-86 15-jul-04 Found SB 181 part 2 PCW.
FAA, U.S AD 86-20-
01
To assure anti-ice capability of pitot
SB 020/34-005, SB 053A
LFV LVD2015 Rev B, MAI SR 020/34-005,
MITSUBISHI SR 053A
06-Oct-
1986
19-May-
2000
FAA, U.S AD 86-26-
02
To prevent engine flameout in an
iceing SB 74-0003, SR 040/74-001
GARRETT SB 74-0003 Rev 6 MAI SR
040/74-001 MITSUBISHI SB 226 Rev E
MITSUBISHI SR 066
31-dec-87 09-mar-09 see applicable engine for c/o
FAA, U.S AD 87-04-
03
Addit. Seal and Flap Flexible Shaft
Insp SB 051/27-007, SB 198
MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 08-jul-85
FAA, U.S AD 87-12-
02
Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 04-May-
1990
FAA, U.S AD 88-13-01
Bendix Autopilot Disengagement SB 066/22-006
LFV LVD2190 MAI SB 066/22-006 Rev A MITSUBISHI SB 206
11-jul-98 06-feb-89 N/A N/A due to Autopilot model
FAA, U.S AD 88-21-01
1 To minimize confusion in autopilot/manua SB 066/22-006
LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-12
FAA, U.S AD 88-23-01
To prevent flap control failure SB 067/27-008, SB 189B
LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 23-mar-95
FAA, U.S AD 93-07-
11
ELECTRIC TRIM SYSTEM SB 079/27-
010
LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n
FAA, U.S AD 94-04-
16
Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 11-mar-93
FAA, U.S AD 94-11-
04
Change of Flight Idle Blade Angel SB
016/61-001
LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n
FAA, U.S AD 96-25-
02
Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-
4552-96 LFV LVD2749
27-dec-96 01-jan-97
FAA, U.S AD 97-04-
13
Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-
1997
N/A N/A due to s/n.
FAA, U.S AD 97-20-
14 CNL
Icing related incidents/accidents 17-Oct-
1997
02-dec-98
FAA, U.S AD 97-25-
02
To prevent loss of airplane
ctrl/overspe
FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17
FAA, U.S AD 98-20-
39
Forward fitting bolt of wingtip tank SB
MU-2 225, 089/57-002A
LFV LVD2688, MITSUBISHI SB 225 19-Oct-
1998
28-jan-97
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
106(195)
FINNISH, Finnish Civil
Aviation Adm.
FINNISH AD M
1177/83
Kontroll av rören till strobe-kablarna MITSUBISHI SB 174 PART 1 Rev C 07-jul-83 20-aug-10
FINNISH AD M
2609/98
Justering av br,nslefl"de MHI SB
097/73-001, TCD-4890-98
JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 02-sep-10
FINNISH AD M
3076
Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 MAI SB 087/56-
001 Rev B MITSUBISHI SB 224 Rev C
21-aug-03 20-aug-10
GARMIN, Garmin
GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 24-May-2010
GARMIN SSB 0845 IR Software Version 6.04 EASA SIB2008-58R 14-nov-08 0 24-May-
2010
GARRETT,
AlliedSignal
Aerospace
GARRETT SB 74-0003
6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 6 09-mar-09 see applicable engine for c/o
HARTZELL, Hartzell
Propeller Inc.
HARTZELL SB 61-256
Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI SL 080
08-feb-02 26-mar-02 R/H
HARTZELL SB 61-279 ALERT
4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL 085
04-Oct-2005
14-nov-05 Propellerbolts previously checked u/a
HARTZELL SB A61-313
3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , MITSUBISHI SL 088 Rev A
15-jul-09 3 20-sep-10 N/A by SSB 0844
HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 Rev A
30-mar-05 9 13-mar-08 see previously revision
JCAB, Japan Civil Aviation
Bureau
JCAB AD TCD- Rivet holes elevator hinge fitting 06-feb-68 26-mar-09 N/A by s/n
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
107(195)
0518-68
JCAB AD TCD-
0642-70
AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 11-mar-86
JCAB AD TCD-
0643-70
Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A N/A by s/n.
JCAB AD TCD-
0652-70
Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-
0653-70
Engine Nacelle Tail Area-Modification
of
25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-
0660-70
Replacement of bearing in
nosegearstrut
LFV LVA457 MITSUBISHI SB 123 01-May-
1970
26-mar-09 N/A by s/n
JCAB AD TCD-0730-1-72
Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev B
25-mar-72 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-0730-2-86
Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n
JCAB AD TCD-0859-72
Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to s/n.
JCAB AD TCD-0866-72
NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-1972
31-dec-72 N/A N/A due to s/n.
JCAB AD TCD-0947A-74
Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev A
12-nov-74 24-Oct-1986
N/A N/A due to s/n.
JCAB AD TCD-0948A-1-78
Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09
JCAB AD TCD-0948A-74
Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev B
07-Oct-1974
01-apr-76
JCAB AD TCD-1001A-76
Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev E
06-Oct-1976
11-mar-86
JCAB AD TCD-1001B-2-84
Replacement of Elevator Trim Tab Bracket
FINNISH AD M 1080/82 LFV LVD1971 MITSUBISHI SB 176 Rev E
12-dec-84 11-mar-86
JCAB AD TCD-
1094A-76
Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A
MITSUBISHI SB 167 Rev D
06-sep-76 06-May-
1977
Revision C PCW by Swedair.
JCAB AD TCD-
1188-75
Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012
MITSUBISHI SB 168 Rev A
06-May-
1975
24-feb-75
JCAB AD TCD-
1202-75
Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A
MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW.
JCAB AD TCD-1209-75
Insp/mod of NLG shimmydamper locking
LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 25-jun-75
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
108(195)
JCAB AD TCD-
1235-75
Insp./repl. of MLG fwd door
emerg.cables
LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 19-feb-86 N/A N/A due to model.
JCAB AD TCD-
1272-75
Supp.,MLG Forward D. Actuating
Mech.-I&M
MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model
JCAB AD TCD-
1284-1-76
Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173
JCAB AD TCD-1328-76
Fire hazard in rear baggage compartment
01-jul-76 26-mar-09 N/A by s/n
JCAB AD TCD-
1353-76
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by s/n
JCAB AD TCD-
1370-76
Inspect strobelight conduit in Tiptank LFV LVA1196 18-Oct-
1976
28-aug-86 Part.1
JCAB AD TCD-
1370A-81
Inspect strobelight conduit in Tiptank
supersed TCD-1370-76
MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 20-aug-10
JCAB AD TCD-
1379-1-80
Insp. rear eng. cowling reg.
heatdamage
LFV LVA1197 Rev A MITSUBISHI SB 177
Rev B
06-feb-02 06-May-
1977
Previously complied with
JCAB AD TCD-
1520A-77
Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180
JCAB AD TCD-
1768-1-85
Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.
JCAB AD TCD-
1817-79
Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
JCAB AD TCD-
2048-81
Insp. firewarning & emerg.power
circuit
LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-
1985
N/A N/A due to model.
JCAB AD TCD-
2070-81
Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 24-nov-81
JCAB AD TCD-
2113-82
Insp./replace engine electrical
harness
LFV LVA1788 MITSUBISHI SB 191 06-feb-02 15-feb-82
JCAB AD TCD-
2252-2-88
Flap system torquetubes supersed
TCD-2252-1-87
01-feb-89 24-mar-09 PCW
JCAB AD TCD-
2252-83
Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 23-mar-95
JCAB AD TCD-
2263-83
NLG. bracket attaching to drag strut 13-aug-83 24-mar-09 N/A by model
JCAB AD TCD-2342-1-84
Engine inlet anti-ice tubing. Torq./lock
MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW
JCAB AD TCD-2342-84
Engine inlet anti-ice tubing. Torq./lock
LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 04-jun-84
JCAB AD TCD-2450A-87
Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
109(195)
JCAB AD TCD-
2451-1-87
Add. seal/Tq. insp of flap flex. shaft 01-May-
1987
09-mar-09 PCW see TCD-2451-85
JCAB AD TCD-
2451-85
Add. seal/Tq. insp of flap flex. shaft
Superseeded by TCD-2451-1-87
LFV LVD2037 MITSUBISHI SB 198 30-sep-85 08-jul-85
JCAB AD TCD-
2545-1-88
Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 06-feb-89
JCAB AD TCD-2679A-97
Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 MITSUBISHI SB 226 Rev E
01-feb-97 22-nov-01
JCAB AD TCD-
3378-90
Insp./mod. of rudder trimtab
leadingedge
LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
3393A-96
Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev
1 MITSUBISHI SB 212 Rev A
25-May-
1996
20-aug-10
JCAB AD TCD-
3464-91
Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model
JCAB AD TCD-
3740A-98
Mod.of Autopilote pitchtrimsystem
MSB 216, 228 LVD 2898
FINNISH AD M 2581/98 LFV LVD2450 LFV
LVD2898 MITSUBISHI SB 216 MITSUBISHI
SB 228
17-aug-98 24-nov-98
JCAB AD TCD-3901-93
Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 MITSUBISHI SB 221
10-sep-93 13-jun-94
JCAB AD TCD-3942-1-94
Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 MITSUBISHI SB 219 Rev A
28-nov-94 23-mar-95
JCAB AD TCD-3942-94
Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 23-mar-95
JCAB AD TCD-
4310-96
Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688
MITSUBISHI SB 225
01-apr-96 28-jan-97
JCAB AD TCD-
4311-95
Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678
MITSUBISHI SB 224 Rev C
01-nov-95 20-aug-10
JCAB AD TCD-
4379-96
Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689
MITSUBISHI SB 229
01-apr-96 30-jul-96
JCAB AD TCD-
4552-96
Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 01-jan-97
JCAB AD TCD-
4625-97
Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB
093/22-009
14-jul-97 04-jun-02
JCAB AD TCD-
4625A-2001
Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B
NYGE TDM01-45
16-mar-01 14-jun-02 PCW Ref AMOC LFV Appr M15/01, TDM 01-45
JCAB AD TCD-
4626-97
De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800
MITSUBISHI SB 232 Rev A
01-May-
1997
14-jul-04
JCAB AD TCD-
4684-97
Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819
MITSUBISHI SB 230
01-jun-97 25-mar-99
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
110(195)
JCAB AD TCD-
4753-98
Ändring av flyghandbok LVD
2922,FAA AD 97-20-14, MHI SN 117A
FINNISH AD M 2518/98 LFV LVD2922
MITSUBISHI SN 117 Rev D
18-feb-98 02-dec-98 FAA AD utförd.
JCAB AD TCD-
4753A-2004
Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 09-jun-04 Inserted in AFM Limitation Section
JCAB AD TCD-
4838-98
Inspection of landing gear power
train
FINNISH AD M 2574/98 LFV LVD2897
MITSUBISHI SB 235
04-aug-98 24-mar-09 N/A by model
JCAB AD TCD-4889-2-2007
Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.
JCAB AD TCD-
4889-98
Insp. of Engine Torque Indication
System LFV 2924, MU SB 233
FINNISH AD M 2608/98 LFV LVD2924
MITSUBISHI SB 233 Rev B
05-nov-98 14-jul-04 PCW
JCAB AD TCD-
4890-98
Check of flight idle FF LVD 2925, MU
SB 234
FINNISH AD M 2609/98 LFV LVD2925
MITSUBISHI SB 234
04-nov-98 13-sep-10
JCAB AD TCD-
5030-99
Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-
1999
24-mar-09 N/A by model
JCAB AD TCD-
5432-2000
AFM revision LFV LVD3112 27-nov-00 12-feb-02
JCAB AD TCD-
5547-2001
To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02
JCAB AD TCD-
5747-2001
Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 27-sep-01
JCAB AD TCD-
5864-2001
Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 16-jan-02
JCAB AD TCD-
6127-2003
Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 12-jun-03
JCAB AD TCD-
7030-2006
Inspection of Wing Attachment
Hardware
MITSUBISHI SB 241 Rev A 27-dec-06 17-jan-07 c/o in conjunction with wingstudie
LFV,
Luftfartsverket
LFV LVA 1011 A Kontroll av vingklaffarnas
manöversystem
FAA, U.S AD 75-16-13 JCAB AD TCD-
1094A-76 MITSUBISHI SB 167 Rev D
05-feb-02 A 06-May-
1977
Revision C PCW by Swedair.
LFV LVA 1012 Kontroll av propellerreglagets
montering
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-
75 MITSUBISHI SB 168 Rev A
05-feb-02 24-feb-75
LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169
Rev B
05-feb-02 25-jun-75
LFV LVA 1014 A Kontr. & byte av motorinkl.
låsanordning
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
05-feb-02 A 30-dec-77
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
111(195)
LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170
Rev A
05-feb-02 19-feb-86 N/A N/A due to s/n.
LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174
PART 1 Rev C
06-feb-02 20-aug-10
LFV LVA 1197 A Förhindr. av värmeskador på
bak.motorpl.
JCAB AD TCD-1379-1-80 MITSUBISHI SB
177 Rev B
06-feb-02 A 06-May-
1977
Previously complied with
LFV LVA 1238 Kontr. & byte av infästningsdet. trimrod
06-feb-02 21-apr-09 N/A by s/n
LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-
1-85 MITSUBISHI SB 181 PART 2 Rev B
06-feb-02 29-nov-84
LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
LFV LVA 1740 Kontr.av brandvarnings-och n"dstr"mskret
JCAB AD TCD-2048-81 MITSUBISHI SB 187 Rev B
05-feb-02 31-aug-09 N/A by s/n
LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 24-nov-81
LFV LVA 1788 Kontroll/Utbyte av elledningar på
motor
JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 15-feb-82
LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB 189
Rev C
06-feb-02 23-mar-95
LFV LVA 1942 Momentdragning/låsn.av koppl.i varmlufts
JCAB AD TCD-2342-84 MITSUBISHI SB 196 Rev A
06-feb-02 04-jun-84
LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 11-mar-86 N/A N/A by s/n
LFV LVA 439 Rev. av flyghandbok betr.
bränslespec.
JCAB AD TCD-0642-70 MITSUBISHI SB 112
Rev C
05-feb-02 11-mar-86
LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model
LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n
LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.
LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 08-dec-09 N/A by A/C serial number
LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n
LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB
162 Rev A
05-feb-02 A 24-Oct-
1986
N/A N/A due to s/n.
LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-
06 JCAB AD TCD-0948A-74 MITSUBISHI SB
163 Rev B
05-feb-02 A 01-apr-76
LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 11-mar-86
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
112(195)
LFV LVD 1238 Kontr./byte infästn.det.
höjdtrimroder
15-apr-77 31-aug-09 N/A by s/n
LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB
176 Rev E
18-jan-85 29-mar-85
LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005
Rev A, MHI SR 53
FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 MAI SR 020/34-005 MITSUBISHI SR 053A
24-May-
1985
B 06-nov-86
LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 08-jul-85
LFV LVD 2069 Altimeter 25-mar-86 23-May-1986
N/A N/A by p/n & s/n
LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA
26-jan-87 25-mar-87
LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006
och SB 206
FAA, U.S AD 88-13-01 MAI SB 066/22-006
Rev A MITSUBISHI SB 206
19-aug-88 06-feb-89 N/A Bendix A/P ej installerad
LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB
201 Rev A
19-aug-88 06-feb-89
LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-
1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C
08-dec-88 23-mar-95
LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-dec-88 12-feb-02
LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB
211
JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
LFV LVD 2347 1 Control Deice-system Mitsubishi SB 212A
JCAB AD TCD-3393A-96 MITSUBISHI SB 212 Rev A
29-May-1996
1 20-aug-10
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9
23-May-1991
04-nov-91 checked OK.
LFV LVD 2450 Elevator Trim Tab Installation MU SB 216
JCAB AD TCD-3740A-98 MITSUBISHI SB 216
03-dec-92 11-mar-93
LFV LVD 2477 Electric Trim System AD930711, MU SB 079/27-0-010
FAA, U.S AD 93-07-11 MAI SB 079/27-010 03-jun-93 27-mar-09 N/A by s/n
LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 13-jun-94
LFV LVD 2537 Reducering av Höjdrodrets
trimområde. FAA AD 94-04-16, SB
216
FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 11-mar-93
LFV LVD 2538 Byte Låspinne i landställets nödutf. SB
219
JCAB AD TCD-3942-94 MITSUBISHI SB 219
Rev A
07-apr-94 23-mar-95
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2012-12-06
Document number Page
113(195)
LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n
LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox
TCD-3942-1-94, MSB 219A
JCAB AD TCD-3942-1-94 MITSUBISHI SB
219 Rev A
09-feb-95 23-mar-95
LFV LVD 2678 Kontr. av vindrutor och fönster MHI
SB 224 Rev A
FAA, U.S AD 2003-17-04 JCAB AD TCD-
4311-95 MITSUBISHI SB 224 Rev C
12-mar-96 20-aug-10
LFV LVD 2688 Kontr/byte av infästn.bult för tiptank
MU-2 SB 225
FAA, U.S AD 98-20-39 JCAB AD TCD-4310-
96 MITSUBISHI SB 225
09-May-
1996
28-jan-97
LFV LVD 2689 Kontroll av linkage för prop.flöjning
MU-2 SB 229
JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-
1996
30-jul-96
LFV LVD 2732 Inspection/ Replacement of Prop
Hub. FAA AD 96-18-14, Hz SB 136H
FAA, U.S AD 96-18-14 HARTZELL SB 61-
261 Rev 1
27-sep-96 04-Oct-
1999
Prop. utbytt mot BVA
LFV LVD 2749 Revision av flyghandbok AFM TCD-4552-96
FAA, U.S AD 96-25-02 JCAB AD TCD-4552-96
21-jan-97 12-feb-02
LFV LVD 2761 Installation av autoignition system TCD-2679A-97
JCAB AD TCD-2679A-97 MITSUBISHI SB 226 Rev E
14-feb-97 29-sep-99
LFV LVD 2769 Demont.av backventil i bränslesystemets MU-2 SB 130A
FAA, U.S AD 97-04-13 MITSUBISHI SB 130 Rev A
18-mar-97 05-May-1997
N/A N/A due to s/n.
LFV LVD 2800 Mod. av De-ice Monitoring System Mitsubishi SB 232, TCD-4626-97
JCAB AD TCD-4626-97 MITSUBISHI SB 232 Rev A
28-aug-97 10-jun-98
LFV LVD 2819 Mod.av lagerboxar för landställssystem Mitsubishi SB 230
JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 23-jun-98
LFV LVD 2853 Periodisk funktionskontroll av nödutgång
23-mar-98 17-dec-09
LFV LVD 2897 Kontroll av landst,llets drivsystem TCD-4838-98, SB 235
JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model
LFV LVD 2898 Mod. av autopilotens höjdtrimsystem TCD-3740A-98, SB 216, 228
JCAB AD TCD-3740A-98 MITSUBISHI SB 216 MITSUBISHI SB 228
27-aug-98 24-nov-98
LFV LVD 2922 Änd.av Flyghandbok-Extra krav på typutbi TCD-4753-98, MHI SN 117A
JCAB AD TCD-4753-98 MITSUBISHI SN 117 Rev D
12-nov-98 02-dec-98 FAA AD utförd.
LFV LVD 2924 Kontr/Just av motorernas Torque
indikeri MHI SB 233, TCD-4889-98
JCAB AD TCD-4889-98 MITSUBISHI SB 233
Rev B
01-dec-98 12-apr-99
LFV LVD 2925 Kontr/just av mot bränsleflöde Flight
Id MHI SB 234
JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 02-sep-10
LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209
Rev B
18-jun-99 24-mar-09 N/A by model
LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02
LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-
009 MITSUBISHI SB 231 Rev B NYGE
02-apr-01 14-jun-02 Ref AMOC LFV Appr M15/01, TDM 01-45
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TDM01-45
LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02
LFV LVD 3166 Sprickkontroll av infästning till ving-spetstank
JCAB AD TCD-5747-2001 MITSUBISHI SB 236
20-sep-01 27-sep-01
LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-012 MITSUBISHI SB 237
09-jan-02 16-jan-02
LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB
239
21-mar-03 12-jun-03
MAI, Mitsubishi Aircraft
International
MAI SB 047/30-001
A Torque of Bleed Air Tube Coupling Nuts AD 84-12-04,SB 196A
FAA, U.S AD 84-12-04 MITSUBISHI SB 196 Rev A
19-jul-84 A 04-jun-84
MAI SB 051/27-
007
Add.Seal and Flap Flexible Shaft
Torque AD 87-04-03, SB 198
FAA, U.S AD 87-04-03 01-feb-85 08-jul-85
MAI SB 067/27-
008
A Insp/Repl. of Flap Control System
Torque AD 88-23-01, SB 189B
FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 23-mar-95
MAI SB 069/24-
006
Split Radio Bus Inspection and
Rework
MAI SB 066/22-006 Rev A 17-nov-88 06-feb-89 N/A N/A due to Aircraft s/n
MAI SB 086/74-
002
A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD
M 2435/97 MITSUBISHI SB 226 Rev E
05-Oct-
2000
A 22-nov-01 Action not required due to s/n.
MAI SB 089/57-
002
A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 28-jan-97 N/A N/A due to s/n.
MAI SN 110/00-017A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MAI SN 111/77-004
Torque Indicating System Shift Potential
20-nov-08 11-mar-09 SB 233 considered
MAI SR 020/34-005
Anti Ice Capability AD 86-20-01, SR 053A
FAA, U.S AD 86-20-01 LFV LVD2015 Rev B MITSUBISHI SR 053A
06-Oct-1986
19-May-2000
N/A N/A due to s/n.
MITSUBISHI,
Mitsubishi Heavy
Industries Ltd
MITSUBISHI MSB
24-004
**RECOVERED RECORD** 19-feb-86 N/A
MITSUBISHI MSR
020
**RECOVERED RECORD** 06-nov-86
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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MITSUBISHI MSR
066
B **RECOVERED RECORD** 25-mar-87 B
MITSUBISHI SB 066 Bendix M4D 18-dec-87 06-feb-89 N/A
MITSUBISHI SB
076/22-008
M-4() Autop.Engage Switch Guard
Install.
11-apr-91 12-apr-95 N/A
MITSUBISHI SB 112 C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-
1971
C 11-mar-86
MITSUBISHI SB 114 Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.
MITSUBISHI SB 119 The Bolt and Bolt Hole Diam. of Nose
L.G
JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model
MITSUBISHI SB 123 Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n
MITSUBISHI SB 124 Scissors Switch,Nose L.G. -Install. of 31-aug-70 19-feb-86 N/A
MITSUBISHI SB 128 B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n
MITSUBISHI SB 143 B Top Coating, Wing Integral Main F.T.-SIo
JCAB AD TCD-0730-1-72 JCAB AD TCD-0730-2-86
05-jan-72 B 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 152 Air Conditioning System-Improvement of
08-nov-71 13-jun-03 N/A N/A by s/n
MITSUBISHI SB 162 A Flex. Shafts, Flap Control Sys.-Insp. of (AD750201)
JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-1974
A 24-Oct-1986
N/A
MITSUBISHI SB 163 B Insp. of Outer Pane, Front Winds. & Inst
FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A
16-nov-78 01-apr-76
MITSUBISHI SB 165 A Lubr. Interval,Wheel Bearing,Main & Nose
24-jul-80 19-feb-86 N/A
MITSUBISHI SB 166 Wing Flap 24-jul-80 11-mar-86 N/A
MITSUBISHI SB 167 D Flap M.Jack Screw-Insp. of and/or Main G
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 LFV LVA1011 Rev A
24-jul-80 D 06-May-1977
Revision C PCW by Swedair.
MITSUBISHI SB 168 A Propeller Pitch Control Lever-Insp. of (AD761620)
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 LFV LVA1012
24-jul-80 A 24-feb-75
MITSUBISHI SB 169 B Shimmy Damper-Insp. and Modification of
JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW
MITSUBISHI SB 170 A MLG Forward Door Em.Op. Cable-Insp. & Re (AD762204)
JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 19-feb-86 N/A N/A due to s/n
MITSUBISHI SB 171 B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 LFV LVA1014 Rev A
17-nov-77 B 30-dec-78
MITSUBISHI SB 173 A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 01-apr-76
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MITSUBISHI SB 174
PART 1
C Tip Tank Conduit Tube-Insp.of,and
Rew.of (AD830902)
FINNISH AD M 1177/83 JCAB AD TCD-
1370A-81 LFV LVA1196
02-Oct-
1981
C 20-aug-10
MITSUBISHI SB 175 Barrel Nut, Inner/Outer Wing Conn.-
Repl.
JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by s/n
MITSUBISHI SB 176 E Elevator Trim Tab Bracket-Repl. of
LVD1971, AD 84-25-02, SB 031/27-005R1
FAA, U.S AD 84-25-02 FINNISH AD M
1080/82 JCAB AD TCD-1001A-76 JCAB AD TCD-1001B-2-84 LFV LVD1971
26-sep-84 E 11-mar-86
MITSUBISHI SB 177 B Mod. of Engine Nacelle Tail Area
(AD810601)
JCAB AD TCD-1379-1-80 LFV LVA1197 Rev
A
11-sep-80 B 06-May-
1977
Previously complied with
MITSUBISHI SB 179 Rodd Assem., Engine Nacelle Upper
D.-R&M
27-May-
1977
10-mar-88
MITSUBISHI SB 180 A Link, Engine Nacelle Upper D.-Repl. of
(AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A
17-nov-77 A 30-dec-77
MITSUBISHI SB 181 PART 2
B Insp. and Repl. of Nose L.G. Strut Assem (AD801812)
FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 LFV LVA1546
08-apr-85 B 29-nov-84
MITSUBISHI SB 182 Add. of Ceiling Cover, Rear Bagg. Comp.
JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n.
MITSUBISHI SB 184 Turnbuckle, Control Cables -Repl. of 04-apr-80 19-feb-86 N/A
MITSUBISHI SB 188 Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 24-nov-81
MITSUBISHI SB 189 C Flap Control Torque Tube AD 88-23-01, SB 067/27-008
FINNISH AD M 2722/00 JCAB AD TCD-2252-1-87 JCAB AD TCD-2252-83 LFV
LVA1873 LFV LVD2202
28-jun-94 C 23-mar-95
MITSUBISHI SB 190 A Trav. Nut Repl. of L.G. Mech. Stop Assem
28-jun-94 23-jul-82
MITSUBISHI SB 191 Engine El. Wire-Insp. and Replacement of (AD820802)
JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 15-feb-82
MITSUBISHI SB 193 B Landing Gear Warning Horn Syst.Modif.
15-jun-94 B 04-dec-00 Rev A är utförd.
MITSUBISHI SB 194 Master Cauting Light Visibility-Impr. of
23-aug-82 14-feb-83
MITSUBISHI SB 196 A Ret. of coupling nut on the bleed air tu AD 84-12-04, SB 047/30-001
FAA, U.S AD 84-12-04 JCAB AD TCD-2342-1-84 JCAB AD TCD-2342-84 LFV LVA1942
MAI SB 047/30-001 Rev A
12-apr-84 A 04-jun-84
MITSUBISHI SB 198 Add. Seal & Torque Insp. of Flap
Flex.Sh LVD2037, AD 87-04-03, SB
051/27-007
FAA, U.S AD 87-04-03 JCAB AD TCD-2451-
85 LFV LVD2037
13-feb-85 08-jul-85
MITSUBISHI SB 199 A Engine Lubricating Tubing Insp. &
Protec
24-jun-94 A 06-nov-09 PCW
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2012-12-06
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MITSUBISHI SB 200 B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 09-aug-88
MITSUBISHI SB 201 A Generator Circuit Wires Insp. and
Mod.
FAA, U.S AD 87-12-02 JCAB AD TCD-2545-
1-88 LFV LVD2191
02-mar-88 A 04-May-
1990
MITSUBISHI SB 204 Speed Placard Change 03-mar-87 13-jun-88
MITSUBISHI SB 206 Bendix Autop.Disengagement Method Stand.
FAA, U.S AD 88-13-01 JCAB AD TCD-2856-1-97 LFV LVD2190
13-Oct-1987
31-jan-89 N/A N/A due to Autopilot model
MITSUBISHI SB 207 Rudder T.T. & Elevator T.T. Insp. &
Rep.
20-May-
1988
17-dec-09
MITSUBISHI SB 209 B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model
MITSUBISHI SB 210 A Engine Ignition Unit Replacement 12-nov-96 06-mar-98
MITSUBISHI SB 211 Rudder Trim Tab Modification (LVD
2338)
JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 212 A Insp of Anti-ice/Deice Systems (LVD
2347),
JCAB AD TCD-3393A-96 LFV LVD2347 Rev
1
25-apr-96 A 20-aug-10
MITSUBISHI SB 214 Engine Control Rod Inspection 06-dec-91 11-mar-93
MITSUBISHI SB 215 Removel of Prop. Governor Speed Signal
23-Oct-1991
30-jan-92 N/A N/A due to -1 engine
MITSUBISHI SB 216 Elevator Trim Tab Installation (LVD 2450
FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV LVD2450
11-sep-92 11-mar-93
MITSUBISHI SB 218 A Propeller Feathering Linkage Inspection
17-jan-94 A 18-feb-94
MITSUBISHI SB 219 A Emergency Gear Down G.box Lower Pin Repl
JCAB AD TCD-3942-1-94 JCAB AD TCD-3942-94 LFV LVD2538 LFV LVD2592
24-Oct-1994
A 23-mar-95
MITSUBISHI SB 221 Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 13-jun-94
MITSUBISHI SB 222 Fuselage Waterproof Modification SR 019
28-jun-94 30-sep-98
MITSUBISHI SB 223 Pitot/Static System Improvement SR 064
MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 19-May-2000
MITSUBISHI SB 224 C Acrylic Windsheild/Window glass Insp. UHB
FAA, U.S AD 2003-17-04 FINNISH AD M 3076 JCAB AD TCD-4311-95 LFV LVD2678
30-apr-98 C 20-aug-10
MITSUBISHI SB 225 Forward fitting bult of wingtip tank LVD 2688
FAA, U.S AD 98-20-39 FINNISH AD M 2351/96 JCAB AD TCD-4310-96 LFV
LVD2688
29-sep-95 28-jan-97
MITSUBISHI SB 226 E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97
FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97
18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n.
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2012-12-06
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FINNISH AD M 2786/00 JCAB AD TCD-
2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A
MITSUBISHI SB 227 Rudder Torque Tube Modification 20-dec-96 23-jun-98
MITSUBISHI SB 228 Elevator Trim Indicator Modification LFV 2898
FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV
LVD2898
13-jul-98 24-nov-98
MITSUBISHI SB 229 Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689
20-feb-96 23-jun-98
MITSUBISHI SB 230 Mod.of Bearing Box Ldg. Gear Act. LVD 2819
JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 23-jun-98
MITSUBISHI SB 231 B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M
2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45
11-dec-02 B 03-mar-03 SL 079 performed earlier.
MITSUBISHI SB 232 A De-Ice System Modification LVD 2800, TCD-4626-97
FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2786/00 JCAB AD TCD-4626-97 LFV
LVD2800 MAI SB 096/30-004
06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev 0.
MITSUBISHI SB 233 B Insp.of Engine Torque Indication
System. TCD-4889-98, LFV 2924
FAA, U.S AD 2006-17-01 FINNISH AD M
2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924
08-mar-07 B 18-apr-07 Checked, previously carried out
MITSUBISHI SB 234 Fl.Check of the Flight Idle Fuel Flow
Se TCD-4890-98, LVD 2925
FAA, U.S AD 2006-17-05 JCAB AD TCD-
4890-98
07-Oct-
1998
02-sep-10
MITSUBISHI SB 235 Inspection of landing gear power
train
JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model
MITSUBISHI SB 236 Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 27-sep-01
MITSUBISHI SB 237 Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 16-jan-02
MITSUBISHI SB 238 Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.
MITSUBISHI SB 239 Pneumatic Line Insp. and Modification
JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 12-jun-03
MITSUBISHI SB 240 Inst.of Trottle Quadrant Placard 26-feb-03 12-jun-03
MITSUBISHI SB 241 A Inspection of Wing Attachment
Hardware
FAA, U.S AD 2006-13-15 JCAB AD TCD-
7030-2006
21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie
MITSUBISHI SL 060 System 17-feb-89 04-nov-91
MITSUBISHI SL 078 Automatic Autopilot Disconnect 28-jan-02 20-aug-10
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2012-12-06
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119(195)
System
MITSUBISHI SL 079 Diode inst.in Flap Position Ind.Curcuit 28-jan-02 14-jun-02
MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.
MITSUBISHI SL 084 Pneumatic De-Ice Monitoring System 14-jun-04 20-aug-10
MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-2005
14-sep-05
MITSUBISHI SN 053
B Rudder Torque Tube AD 86-20-01, SB 020/34-005
05-nov-86 B 12-jun-87
MITSUBISHI SN 117
D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD TCD-4753-98
14-jun-04 D 09-jun-04
MITSUBISHI SN
146
Water Ingress into Vertical Stabilizer 19-dec-03 09-jun-04
MITSUBISHI SN
148
Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB
MITSUBISHI SN
156A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MITSUBISHI SN
157
Torque Indicating System Shift
Potential
20-nov-08 11-mar-09 SB 233 considered
MITSUBISHI SN
161
Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE
MITSUBISHI SR
053A
Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 LFV LVD2015 Rev B MAI SR 020/34-005 MITSUBISHI SB 223
23-Oct-
1984
14-nov-86
MITSUBISHI SR 064 Pitot & Static System MITSUBISHI SB 223 30-apr-85 19-May-2000
MITSUBISHI SR 065 Warning Horn 20-jan-86 13-jun-88
MITSUBISHI SR 067 Emergency Exit Placard 17-sep-85 15-jan-86
MITSUBISHI SR 072 Air Filter Replacement for Vacuum Syst.
25-apr-00 29-jan-01
MITSUBISHI SR 075 Inst. tip tank placard 29-Oct-2004
02-May-2005
MITSUBISHI STC SA01913SE
Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-09 11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection
NARCO, Narco
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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120(195)
NARCO SB ELT10-
16
ELT ASSY 18-apr-88 04-nov-91 N/A ELT ASSY
NYGE, Saab Aerotech
Aircraft Services
NYGE TDM 01-45 Installation of Trim-In-Motion Alert
Syst. and Automatic A/P Disconnect syst.
JCAB AD TCD-4625A-2001 LFV LVD3122
MITSUBISHI SB 231 Rev B
07-May-
2001
14-jun-02
NYGE TDM 02-10 Installation of TPE331-6-252M Engines
25-mar-02 13-jun-03
NYGE TDM 02-24 Installation Moving MAP 10-Oct-2002
18-dec-02
NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04
NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 install.
04-mar-03 21-Oct-2008
NYGE TDM 03-12 Installation Ugglan 25-mar-03 07-apr-03
NYGE TDM 03-15 A U95 with General Control System 24-apr-03 A 25-feb-08
NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 31-aug-09 Original compliance by Rev D. Not affected by rev F.
NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05
NYGE TDM 05-35 A Installation FR-31 11-May-2006
A 12-May-2006
Approved i.a.w. DOA 21j.108.05-35
NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 18-sep-07
NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06 A 07-feb-08
NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07 A 07-feb-08
NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 29-feb-08
NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 17-dec-09
NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 21-Oct-2008
Original compliance with TDM rev A. Rev B does not affect previous complaiance.
NYGE TDM 09-24 A Electrical Wiring Feed Through 08-sep-09 A 31-aug-09
NYGE TDM 09-31 A GPS Splitter 12-nov-09 A 10-dec-09
NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 01-Oct-2010
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
121(195)
NYGE TDM 10-03 A Pressure Bulkhead Feed Through 04-May-
2010
A 01-Oct-
2010
NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 25-May-
2010
NYGE TDM 11-35 A Terminating resistor A 21-Feb-12
NYGE TDM 12-21 A Avinstallation IK A 4-Jun-12
NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 27-mar-09
NYGE TDM 96-06 Rep. sprickor "hinge,front spar flange"
11-nov-96 14-nov-96
NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 29-sep-99
NYGE TVO 1/09 Inspektion av Stringers & struktur
vinge
25-feb-09 08-apr-09 Inspected with remarks
NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 03-mar-93
NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 20-jun-02
NYGE TVO 1/97 3 De-Icertank MU-2B, korrosionskontroll
12-feb-97 24-jun-98
NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01-dec-00 01-feb-01
NYGE TVO 2/07 A Prevent FR31 radio to xmit when RM2 off
06-feb-07 A 02-mar-07
NYGE TVO 2/91 A/C Elecrical System 10-jan-91 24-jun-92
NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06 20-aug-10
NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 17-dec-09
NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 20-aug-10
NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 24-jun-92
NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 24-jun-92
NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 20-aug-10
NYGE TVO 4/96 Kontroll av Lagerhus i
noshjulsstyrning.
25-Oct-
1996
01-jul-97 Utförd tidigare (ref. Ove N lista)
NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 17-dec-09
NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-
1992
27-Oct-
1992
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
122(195)
NYGE TVO 7/93 Starter Drive Splines 01-nov-93 09-aug-94
NYGE TVO 8/04 Kontr. av Spant vid bakre
feninfästning
08-dec-04 17-dec-09
NYGE TVO 8/92 Wheel Parts 27-Oct-
1992
11-mar-93
NYGE TVO 9/88 Emergency Extension System 08-aug-88 06-feb-89
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
123(195)
2.5 GFE Aircraft Mitsubishi MU-2 SE-GHF
2.5.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
MU-2B-20 299 SE-GHF 12688 6751 2012-11-23
2.5.2 Engines Type: Honeywell TPE331-6-252M
Serial
Number:
Total
Hours
Since New:
Total
Cycles
Since New:
Hours remaining to
overhaul/HIS/GBI:
Left Engine P20388 7806 6761 3101/1288/1301
Right
Engine
P27037 14603 16508 1233/352/2152
2.5.3 Propeller Type Number: Serial Number: Overhaul Due Date:
Left Propeller HC-B3TN-5E BVA 6124 2013-01-26
Right Propeller HC-B3TN-5E BVA 6222 2013-01-29
2.5.4 Avionics System: Type / Part Number: Note:
Autopilot & Flight Director Century IV
COM/NAV/GPS 1 Garmin GNS 530
COM/NAV/GPS 2 Garmin GNS 430
Audiopanel Bendix/King KMA-24H-70
MKR Bendix/King KR-21
DME Bendix/King KDM-706
ADF Bendix/King KDF-806
XPDR 1 Garmin GTX 330D Mode S EHS
XPDR 1 / 2 Garmin GTX 330 *) Mode S EHS
RDR ALT Bendix/King KRA-10A
ELT Kanad ELT 406-AF-H
Airspeed Indicator LH / RH Aerosonic 20040-161 / 20040-
0186
Altimeter LH United Instr. Inc. 5934 PAM-3
Altimeter incl. encoder RH United Instr. Inc. 5035P-P40
Altitude Reporter Narco AR 850
Altitude Alerter Aero Mechanism AM 275C
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
124(195)
Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3
Attitude Gyro & Flight Director Ind.
LH
Century 52C77
Attitude Gyro Ind. RH AIM 504-0006-914
Turn & Bank Ind. LH R.C Allen A5930-02
Horizontal Situation Indicator LH Bendix/King KPI-553A
DG-Gyro Sperry C-14A
Directional Gyro RMI Ind. LH AIM 254-1D
RMI/ADF adapter Bendix/King KDA-692
CDI Indicator Garmin GI-106A
*) XPDR 2 without diversity configuration
2.5.5 Mission System System: Description:
Fixed general installations
VHF/UHF COM 1 & 2 FR31
GPS MAP
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
Laser Prism
MIL-STD-1553 Bus LH Wing Pylon
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ASTOR Fixed installed system
ADRIAN Pod mounted system LH and RH Wing
Pylon
U95 N Pod mounted system LH Wing Pylon
U95 Sorc Pod mounted system RH Wing Pylon U95 Sorc
A100 Pod mounted system LH Wing Pylon
Missile Threat Simulator
DARTS Pod mounted system LH Wing Pylon
Chaff Dispenser
BOX 3 Pod mounted system LH and RH Wing
Pylon
2.5.6 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, U95-N, A100,
DARTS and BOX 3 General Signal Harness AWG22 shielded x 44
General Signal Harness AWG22 shielded x 50
U95-N and A100 MIL-STD-1553B Data
Bus
MIL-STD-1553B Data
Bus
Triax Cable x 1
U95-N, A100 and DARTS AC Power
115/200VAC 400 Hz 3-
AWG 12 x 4
twisted
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
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Phase 3 x 10 A AWG 16 x 2
AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200
A
DC Power 28 VDC 200
A
AWG 2 x 2
Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Coax Cable 1 x 75 Ω Prepared installation Ethernet LAN Cable
2.5.7 Antenna Layout
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
126(195)
2.5.8 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date
Aircraft SE-GHF
Vingstudie MU-2 AMP 2012-05-06 12687 13700
100 Hour Inspection AMP 2012-05-15 12687 12787,1 2013-06-25
200 Hour Inspection AMP 2012-05-14 12687 12887,1 2013-06-25
600 Hour Inspection AMP 2010-09-14 12557 13157,7 2013-09-13
1000 Hour Inspection AMP 2012-05-14 12687 13700
1200 Hour Inspection AMP 11700 12900
1800 Hour Inspection AMP 11400 13200
2000 Hour Inspection AMP 11700 13700
1 Year Inspection AMP 2012-05-31 12687 2013-06-25
2 Year Inspection AMP 2012-06-20 12687 2014-06-25
10 Year Inspection AMP 2004-04-26 11800 2014-04-24
Engine S/N P-20388
Remaining
Engine Assembly (Overhaul) AMP 15789,8 3101,6
Engine Hot Section Inspection AMP 13977 1288,8
Engine Gearbox Inspection AMP 13989,8 1301,6
Engine S/N P-27037
Engine Assembly (Overhaul) AMP 13921,9 1233,7
Engine Hot Section Inspection AMP 13041,1 352,9
Engine Gearbox Inspection AMP 14841,1 2152,9
Propeller L/H O/H AMP 2008-01-08 15177 2013-01-06
Propeller R/H O/H AMP 2008-01-31 15367,5 2013-01-29
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
127(195)
2.5.9 Implemented Changes Status date November 23
rd 2012.
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Compliance Status Remarks
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Complianc
e
Stat
us
Remarks
CENTURY, Century Flight
Systems Inc.
CENTURY SB CSB-
2005-01
Check for frayed Bridle Cable 21-feb-05 15-sep-10
EASA, European Aviation
Safety Agency
EASA AD 2006-0265 Incorrect transponder altitude 30-aug-06 09-dec-10
EASA AD 2009-
0251-E
Portable Fire Extinguishers-
Ident/Repl
25-nov-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-0262 Halon 1211 Fire Extinguishers
Id/Repl
EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2009-0278 Halon 1211 Fire Extinguishers
Id/Repl
EASA AD 2009-0262 22-dec-09 07-May-
2010
N/A N/A by current P/N installed
EASA AD 2010-0003 R1 Mode S Transponder -
Check/Modification
11-jan-10 R1 10-mar-10 N/A due to model
EASA AD 2012-0037 Kidde Graviner hand operated fire
extinguisher
25-Jun-12
EASA SIB 2008-
58R1
Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN
SSB0845 Rev IR
17-dec-08 21-sep-10 N/A by SSB 0845 incorporated
EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
128(195)
FAA, U.S, Federal Aviation Administration
FAA, U.S AD 2000-
02-25
AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b.
FAA, U.S AD 2000-
09-15
1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M
2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004
MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A
07-jul-00 1 23-nov-01
FAA, U.S AD 2003-
17-04
Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB
087/56-001 Rev B MITSUBISHI SB 224 Rev C
01-Oct-
2003
09-sep-10
FAA, U.S AD 2003-22-07
1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-4753A-2004 MAI SN 071/00-006 Rev D
MITSUBISHI SN 117 Rev D
16-apr-04 17-May-2004
inserted in AFM
FAA, U.S AD 2005-14-12
Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 17-sep-08 L/H side
FAA, U.S AD 2005-18-20
Prop de-icer "FASTprop" 14-Oct-2005
12-Oct-2005
N/A Due to boots p/n
FAA, U.S AD 2006-13-15
Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 241 Rev A
11-aug-06 26-apr-04 c/o in conjunction with vingstudie
FAA, U.S AD 2006-15-07
Safety evaluation (feathering linkage)
MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229
FAA, U.S AD 2006-17-01
Detect & correct torque transducers
MAI SB 095/77-002 MITSUBISHI SB 233 Rev B
22-sep-06 21-sep-06 PCW see MSB 233A
FAA, U.S AD 2006-17-05
Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 13-Oct-2010
FAA, U.S AD 2007-17-09
Reduce max deflect elev nose-down trim
MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's.
FAA, U.S AD 71-14-01
Fuel Tank Fungus Coating Peeling 01-May-1972
01-jan-96 N/A N/A by s/n
FAA, U.S AD 74-11-
01
Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
30-jan-78 01-dec-10 PCW See JCAB AD TCD-0948A-1-78
FAA, U.S AD 75-16-
13
Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev
A MITSUBISHI SB 167 Rev D
05-aug-75 03-May-
1977
Revision C PCW by Swedair.
FAA, U.S AD 75-16-
20
Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012
MITSUBISHI SB 168 Rev A
12-aug-75 25-apr-75
FAA, U.S AD 78-03-
05
Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A
MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
23-feb-78 11-aug-75
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
129(195)
FAA, U.S AD 81-06-
01
1 Engine Aft Nacelles 01-apr-81 1 23-jun-97 Previously complied with
FAA, U.S AD 81-25-
04
1 Engine's Electrical wiring SB
036/71-003A, SB 043/71-005
21-jan-82 1 02-dec-10 N/A N/A by model
FAA, U.S AD 82-08-
02
Electrical Wiring Inspection 15-apr-82 25-mar-82
FAA, U.S AD 83-08-01
2 To preclude prop. attach bolt failures
FINNISH AD M 1168/83 Rev 1 FINNISH AD T5114/05 HARTZELL SI 140A Rev 9
28-apr-82 2 20-May-2005
Ref. MU2B MM chap 13.4 when using bolts P/N B-3339 only
FAA US AD 83-09-
02
Strobe light assemblies 16-Mar-12
FAA, U.S AD 84-12-
04
Torque of Air Tube Coupling Nuts
SB 047/30-001, SB 196A
MAI SB 047/30-001 Rev A MITSUBISHI SB
196 Rev A
28-jun-84 19-jun-84
FAA, U.S AD 84-25-
02
Elevator TrimTab Bracket
Insp/Repl. SB 031/27-005 R1, SB
176E
MAI SB 031/27-005 Rev 1 MITSUBISHI SB
176 Rev E
18-dec-84 19-mar-86
FAA, U.S AD 86-15-
03
NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2
Rev B
13-aug-86 15-jul-04 Found SB 181 part 2 PCW.
FAA, U.S AD 86-20-01
To assure anti-ice capability of pitot SB 020/34-005, SB 053A
LFV LVD2015 Rev B, MAI SR 020/34-005 , MITSUBISHI SR 053A
06-Oct-1986
17-May-2004
FAA, U.S AD 86-26-02
To prevent engine flameout in an iceing SB 74-0003, SR 040/74-001
GARRETT SB 74-0003 Rev 6 MAI SR 040/74-001 MITSUBISHI SB 226 Rev E
MITSUBISHI SR 066
31-dec-87 09-mar-09 see applicable engine for c/o
FAA, U.S AD 87-04-
03
Addit. Seal and Flap Flexible Shaft
Insp SB 051/27-007, SB 198
MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 27-jan-83
FAA, U.S AD 87-12-
02
Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 02-Oct-
1990
FAA, U.S AD 88-13-
01
Bendix Autopilot Disengagement SB
066/22-006
LFV LVD2190 MAI SB 066/22-006 Rev A
MITSUBISHI SB 206
11-jul-98 01-sep-89 N/A N/A due to Autopilot model
FAA, U.S AD 88-21-01
1 To minimize confusion in autopilot/manua SB 066/22-006
LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-12
FAA, U.S AD 88-23-01
To prevent flap control failure SB 067/27-008, SB 189B
LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 03-mar-95
FAA, U.S AD 93-07-11
ELECTRIC TRIM SYSTEM SB 079/27-010
LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n
FAA, U.S AD 94-04-16
Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 26-May-1993
FAA, U.S AD 94-11-04
Change of Flight Idle Blade Angel SB 016/61-001
LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n
FAA, U.S AD 96-25-
02
Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-
4552-96 LFV LVD2749
27-dec-96 19-feb-02
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
130(195)
FAA, U.S AD 97-04-
13
Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-
1997
N/A N/A due to s/n.
FAA, U.S AD 97-20-
14 CNL
Icing related incidents/accidents 17-Oct-
1997
02-dec-98
FAA, U.S AD 97-25-
02
To prevent loss of airplane
ctrl/overspe
FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17
FAA, U.S AD 98-20-39
Forward fitting bolt of wingtip tank SB MU-2 225, 089/57-002A
LFV LVD2688 , MITSUBISHI SB 225 19-Oct-1998
30-jan-97
FINNISH, Finnish
Civil Aviation Adm.
FINNISH AD M 1177/83
Kontroll av rören till strobe-kablarna
MITSUBISHI SB 174 PART 1 Rev C 07-jul-83 09-sep-10
FINNISH AD M 2609/98
Justering av br,nslefl"de MHI SB 097/73-001, TCD-4890-98
JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 13-Oct-2010
FINNISH AD M 3076 Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 MAI SB 087/56-001 Rev B MITSUBISHI SB 224 Rev C
21-aug-03 09-sep-10
GARMIN, Garmin
GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 20-May-
2010
GARMIN SSB 0845 IR Software Version 6.04 EASA SIB2008-58R 14-nov-08 0 20-May-
2010
GARRETT,
AlliedSignal
Aerospace
GARRETT SB 74-
0003
6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 6 09-mar-09 see applicable engine for c/o
HARTZELL, Hartzell
Propeller Inc.
HARTZELL SB 61-256
Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI SL 080
08-feb-02 19-mar-02 L/H & R/H side
HARTZELL SB 61-
279 ALERT
4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL
085
04-Oct-
2005
17-sep-08 L/H side
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
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HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424
Rev A
30-mar-05 9 13-mar-08 see previously revision
JCAB, Japan Civil
Aviation Bureau
JCAB AD TCD-0518-
68
Rivet holes elevator hinge fitting 06-feb-68 26-mar-09 N/A by s/n
JCAB AD TCD-0642-
70
AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 17-apr-86
JCAB AD TCD-0643-
70
Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A N/A by s/n.
JCAB AD TCD-0652-70
Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-0653-70
Engine Nacelle Tail Area-Modification of
25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-0660-70
Replacement of bearing in nosegearstrut
LFV LVA457 MITSUBISHI SB 123 01-May-1970
26-mar-09 N/A by s/n
JCAB AD TCD-0730-1-72
Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev B
25-mar-72 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-0730-2-86
Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n
JCAB AD TCD-0859-72
Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to s/n.
JCAB AD TCD-0866-72
NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-1972
31-dec-72 N/A N/A due to s/n.
JCAB AD TCD-0947A-74
Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev A
12-nov-74 21-aug-86 N/A N/A due to s/n.
JCAB AD TCD-0948A-1-78
Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09
JCAB AD TCD-
0948A-74
Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
07-Oct-
1974
15-mar-86
JCAB AD TCD-
1001A-76
Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev
E
06-Oct-
1976
19-mar-86
JCAB AD TCD-
1001B-2-84
Replacement of Elevator Trim Tab
Bracket
FINNISH AD M 1080/82 LFV LVD1971
MITSUBISHI SB 176 Rev E
12-dec-84 19-mar-86
JCAB AD TCD-
1094A-76
Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A
MITSUBISHI SB 167 Rev D
06-sep-76 03-May-
1977
Revision C PCW by Swedair.
JCAB AD TCD-1188-
75
Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012
MITSUBISHI SB 168 Rev A
06-May-
1975
25-apr-75
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
132(195)
JCAB AD TCD-1202-
75
Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A
MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW.
JCAB AD TCD-1209-75
Insp/mod of NLG shimmydamper locking
LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 11-jun-75
JCAB AD TCD-1235-75
Insp./repl. of MLG fwd door emerg.cables
LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 17-apr-86 N/A N/A due to model.
JCAB AD TCD-1272-
75
Supp.,MLG Forward D. Actuating
Mech.-I&M
MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model
JCAB AD TCD-1284-
1-76
Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 01-sep-09 PCW Ref. SB 173
JCAB AD TCD-1328-
76
Fire hazard in rear baggage
compartment
01-jul-76 26-mar-09 N/A by s/n
JCAB AD TCD-1353-
76
Barrel Nut, Inner/Outer Wing
Conn.-Repl.
MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by p/n
JCAB AD TCD-1370-
76
Inspect strobelight conduit in
Tiptank
LFV LVA1196 18-Oct-
1976
21-aug-86 Part.1
JCAB AD TCD-1370A-81
Inspect strobelight conduit in Tiptank supersed TCD-1370-76
MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 09-sep-10
JCAB AD TCD-1379-1-80
Insp. rear eng. cowling reg. heatdamage
LFV LVA1197 Rev A MITSUBISHI SB 177 Rev B
06-feb-02 23-jun-77 Previously complied with
JCAB AD TCD-1520A-77
Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180
JCAB AD TCD-1768-
1-85
Fatigue failure of the NLG strut
assy.
LFV LVA1546 MITSUBISHI SB 181 PART 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.
JCAB AD TCD-1817-
79
Modification of
bagagecompartment
LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
JCAB AD TCD-2048-
81
Insp. firewarning & emerg.power
circuit
LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-
1981
N/A N/A due to model.
JCAB AD TCD-2070-
81
Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 25-mar-82
JCAB AD TCD-2113-
82
Insp./replace engine electrical
harness
LFV LVA1788 MITSUBISHI SB 191 06-feb-02 25-mar-82 Checked N/A due to color (brown) of cables i.a.w.
SB 191
JCAB AD TCD-2252-
2-88
Flap system torquetubes supersed
TCD-2252-1-87
01-feb-89 24-mar-09 PCW
JCAB AD TCD-2252-
83
Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 03-mar-95
JCAB AD TCD-2263-
83
NLG. bracket attaching to drag strut 13-aug-83 24-mar-09 N/A by model
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2012-12-06
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JCAB AD TCD-2342-
1-84
Engine inlet anti-ice tubing.
Torq./lock
MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW
JCAB AD TCD-2342-
84
Engine inlet anti-ice tubing.
Torq./lock
LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 19-jun-84
JCAB AD TCD-
2450A-87
Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.
JCAB AD TCD-2451-1-87
Add. seal/Tq. insp of flap flex. shaft 01-May-1987
09-mar-09 PCW see TCD-2451-85
JCAB AD TCD-2451-
85
Add. seal/Tq. insp of flap flex. shaft
Superseeded by TCD-2451-1-87
LFV LVD2037 MITSUBISHI SB 198 30-sep-85 27-jan-83
JCAB AD TCD-2545-
1-88
Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 02-Oct-
1986
JCAB AD TCD-
2679A-97
Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761
MITSUBISHI SB 226 Rev E
01-feb-97 22-nov-01
JCAB AD TCD-3378-
90
Insp./mod. of rudder trimtab
leadingedge
LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
3393A-96
Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev
1 MITSUBISHI SB 212 Rev A
25-May-
1996
15-sep-10
JCAB AD TCD-3464-
91
Unintentional engagement of
A/P......
17-jun-91 24-mar-09 N/A by model
JCAB AD TCD-
3740A-98
Mod.of Autopilote pitchtrimsystem
MSB 216, 228 LVD 2898
FINNISH AD M 2581/98 LFV LVD2450 LFV
LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228
17-aug-98 08-dec-98
JCAB AD TCD-3901-
93
Tiptank inst FINNISH AD M 2110/93 LFV LVD2512
MITSUBISHI SB 221
10-sep-93 15-mar-94
JCAB AD TCD-3942-
1-94
Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592
MITSUBISHI SB 219 Rev A
28-nov-94 03-mar-95
JCAB AD TCD-3942-
94
Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 03-mar-95
JCAB AD TCD-4310-
96
Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688
MITSUBISHI SB 225
01-apr-96 30-jan-97
JCAB AD TCD-4311-
95
Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678
MITSUBISHI SB 224 Rev C
01-nov-95 09-sep-10
JCAB AD TCD-4379-
96
Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689
MITSUBISHI SB 229
01-apr-96 30-jul-96
JCAB AD TCD-4552-
96
Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 19-feb-02
JCAB AD TCD-4625-
97
Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB
093/22-009
14-jul-97 23-nov-01
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2012-12-06
Document number Page
134(195)
JCAB AD TCD-
4625A-2001
Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B
NYGE TDM01-45
16-mar-01 13-mar-09 PCW Ref AMOC LFV Appr M15/01, TDM 01-45
JCAB AD TCD-4626-
97
De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800
MITSUBISHI SB 232 Rev A
01-May-
1997
14-jul-04 PCW
JCAB AD TCD-4684-
97
Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819
MITSUBISHI SB 230
01-jun-97 25-mar-99
JCAB AD TCD-4753-98
Ändring av flyghandbok LVD 2922,FAA AD 97-20-14, MHI SN
117A
FINNISH AD M 2518/98 LFV LVD2922 MITSUBISHI SN 117 Rev D
18-feb-98 02-dec-98 FAA AD utförd.
JCAB AD TCD-
4753A-2004
Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-
2004
inserted in AFM
JCAB AD TCD-4838-
98
Inspection of landing gear power
train
FINNISH AD M 2574/98 LFV LVD2897
MITSUBISHI SB 235
04-aug-98 24-mar-09 N/A by model
JCAB AD TCD-4889-
2-2007
Inappropriate calib. of eng. trq-
meter
MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.
JCAB AD TCD-4889-
98
Insp. of Engine Torque Indication
System LFV 2924, MU SB 233
FINNISH AD M 2608/98 LFV LVD2924
MITSUBISHI SB 233 Rev B
05-nov-98 14-jul-04 PCW
JCAB AD TCD-4890-98
Check of flight idle FF LVD 2925, MU SB 234
FINNISH AD M 2609/98 LFV LVD2925 MITSUBISHI SB 234
04-nov-98 13-Oct-2010
JCAB AD TCD-5030-99
Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-1999
24-mar-09 N/A by model
JCAB AD TCD-5432-2000
AFM revision LFV LVD3112 27-nov-00 12-feb-02
JCAB AD TCD-5547-
2001
To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02
JCAB AD TCD-5747-
2001
Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 08-Oct-
2001
JCAB AD TCD-5864-
2001
Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 17-jan-02
JCAB AD TCD-6127-
2003
Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 09-Oct-
2003
JCAB AD TCD-7030-
2006
Inspection of Wing Attachment
Hardware
MITSUBISHI SB 241 Rev A 27-dec-06 17-jan-07 c/o in conjunction with wingstudie
LFV, Luftfartsverket
LFV LVA 1011 A Kontroll av vingklaffarnas manöversystem
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 MITSUBISHI SB 167 Rev D
05-feb-02 A 03-May-1977
Revision C PCW by Swedair.
LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 05-feb-02 25-apr-75
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2012-12-06
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135(195)
montering 75 MITSUBISHI SB 168 Rev A
LFV LVA 1013 Kontr. och mod. av låsning på
nosställ
JCAB AD TCD-1209-75 MITSUBISHI SB 169
Rev B
05-feb-02 11-jun-75
LFV LVA 1014 A Kontr. & byte av motorinkl.
låsanordning
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
05-feb-02 A 11-aug-75
LFV LVA 1083 Insp. & utbyte av lina för nödöppning
JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A
05-feb-02 17-apr-86 N/A N/A due to s/n.
LFV LVA 1196 Isolering av strobe light från bränsle
JCAB AD TCD-1370-76 MITSUBISHI SB 174 PART 1 Rev C
06-feb-02 09-sep-10
LFV LVA 1197 A Förhindr. av värmeskador på bak.motorpl.
JCAB AD TCD-1379-1-80 MITSUBISHI SB 177 Rev B
06-feb-02 A 23-jun-77 Previously complied with
LFV LVA 1238 Kontr. & byte av infästningsdet.
trimrod
06-feb-02 21-apr-09 N/A by s/n
LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-
1-85 MITSUBISHI SB 181 PART 2 Rev B
06-feb-02 24-aug-84
LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.
LFV LVA 1740 Kontr.av brandvarnings-och n"dstr"mskret
JCAB AD TCD-2048-81 MITSUBISHI SB 187 Rev B
05-feb-02 31-aug-09 N/A by s/n
LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 25-mar-82
LFV LVA 1788 Kontroll/Utbyte av elledningar på motor
JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 25-mar-82 Checked N/A due to color (brown) of cables i.a.w. SB 191
LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör
JCAB AD TCD-2252-83 MITSUBISHI SB 189 Rev C
06-feb-02 03-mar-95
LFV LVA 1942 Momentdragning/låsn.av koppl.i
varmlufts
JCAB AD TCD-2342-84 MITSUBISHI SB 196
Rev A
06-feb-02 19-jun-84
LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 15-jul-04 N/A N/A by s/n.
LFV LVA 439 Rev. av flyghandbok betr.
bränslespec.
JCAB AD TCD-0642-70 MITSUBISHI SB 112
Rev C
05-feb-02 17-apr-86
LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model
LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp.
JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n
LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.
LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 08-dec-09 N/A by A/C serial number
LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n
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2012-12-06
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LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB
162 Rev A
05-feb-02 A 21-aug-86 N/A N/A due to s/n.
LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-
06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B
05-feb-02 A 26-mar-09
LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar
JCAB AD TCD-1001A-76 05-feb-02 A 19-mar-86
LFV LVD 1238 Kontr./byte infästn.det.
höjdtrimroder
15-apr-77 31-aug-09 N/A by s/n
LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB
176 Rev E
18-jan-85 19-mar-86
LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-
005 Rev A, MHI SR 53
FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 MAI SR 020/34-005 MITSUBISHI SR 053A
24-May-
1985
B 06-Oct-
1986
LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 03-jun-85
LFV LVD 2069 Altimeter 25-mar-86 07-jul-86 N/A N/A by p/n & s/n
LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA
26-jan-87 12-jun-87
LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006 och SB 206
FAA, U.S AD 88-13-01 MAI SB 066/22-006 Rev A MITSUBISHI SB 206
19-aug-88 01-sep-89 N/A Bendix A/P ej installerad
LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB 201 Rev A
19-aug-88 01-sep-89
LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C
08-dec-88 03-mar-95
LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-Dec-1988
12-feb-02
LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB
211
JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
LFV LVD 2347 1 Control Deice-system Mitsubishi SB
212A
JCAB AD TCD-3393A-96 MITSUBISHI SB
212 Rev A
29-May-
1996
1 15-sep-10
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-
13 CHPT 9
23-May-
1991
16-Oct-
1991
checked OK.
LFV LVD 2450 Elevator Trim Tab Installation MU
SB 216
JCAB AD TCD-3740A-98 MITSUBISHI SB
216
03-dec-92 26-May-
1993
LFV LVD 2477 Electric Trim System AD930711, MU SB 079/27-0-010
FAA, U.S AD 93-07-11 MAI SB 079/27-010 03-jun-93 27-mar-09 N/A by s/n
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2012-12-06
Document number Page
137(195)
LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 15-mar-94
LFV LVD 2537 Reducering av Höjdrodrets
trimområde. FAA AD 94-04-16, SB 216
FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 26-May-
1993
LFV LVD 2538 Byte Låspinne i landställets nödutf. SB 219
JCAB AD TCD-3942-94 MITSUBISHI SB 219 Rev A
07-apr-94 03-mar-95
LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04
FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n
LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox TCD-3942-1-94, MSB 219A
JCAB AD TCD-3942-1-94 MITSUBISHI SB 219 Rev A
09-feb-95 03-mar-95
LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB 224 Rev A
FAA, U.S AD 2003-17-04 JCAB AD TCD-4311-95 MITSUBISHI SB 224 Rev C
12-mar-96 09-sep-10
LFV LVD 2688 Kontr/byte av infästn.bult för
tiptank MU-2 SB 225
FAA, U.S AD 98-20-39 JCAB AD TCD-4310-
96 MITSUBISHI SB 225
09-May-
1996
26-jun-00 L/H-side
LFV LVD 2689 Kontroll av linkage för prop.flöjning
MU-2 SB 229
JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-
1996
30-jul-96
LFV LVD 2732 Inspection/ Replacement of Prop
Hub. FAA AD 96-18-14, Hz SB 136H
FAA, U.S AD 96-18-14 HARTZELL SB 61-
261 Rev 1
27-sep-96 16-nov-98 Prop. utbytt mot BVA
LFV LVD 2749 Revision av flyghandbok AFM TCD-
4552-96
FAA, U.S AD 96-25-02 JCAB AD TCD-4552-
96
21-jan-97 19-feb-02
LFV LVD 2761 Installation av autoignition system
TCD-2679A-97
JCAB AD TCD-2679A-97 MITSUBISHI SB
226 Rev E
14-feb-97 15-jun-99
LFV LVD 2769 Demont.av backventil i bränslesystemets MU-2 SB 130A
FAA, U.S AD 97-04-13 MITSUBISHI SB 130 Rev A
18-mar-97 05-May-1997
N/A N/A due to s/n.
LFV LVD 2800 Mod. av De-ice Monitoring System Mitsubishi SB 232, TCD-4626-97
JCAB AD TCD-4626-97 MITSUBISHI SB 232 Rev A
28-aug-97 10-jun-98
LFV LVD 2819 Mod.av lagerboxar för landställssystem Mitsubishi SB 230
JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 21-apr-98
LFV LVD 2853 Periodisk funktionskontroll av nödutgång
23-mar-98 02-feb-11
LFV LVD 2897 Kontroll av landst,llets drivsystem TCD-4838-98, SB 235
JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model
LFV LVD 2898 Mod. av autopilotens höjdtrimsystem TCD-3740A-98, SB
216, 228
JCAB AD TCD-3740A-98 MITSUBISHI SB 216 MITSUBISHI SB 228
27-aug-98 08-dec-98
LFV LVD 2922 Änd.av Flyghandbok-Extra krav på typutbi TCD-4753-98, MHI SN 117A
JCAB AD TCD-4753-98 MITSUBISHI SN 117 Rev D
12-nov-98 02-dec-98 FAA AD utförd.
LFV LVD 2924 Kontr/Just av motorernas Torque indikeri MHI SB 233, TCD-4889-98
JCAB AD TCD-4889-98 MITSUBISHI SB 233 Rev B
01-dec-98 01-apr-99
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
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LFV LVD 2925 Kontr/just av mot bränsleflöde
Flight Id MHI SB 234
JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 13-Oct-
2010
LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209
Rev B
18-jun-99 24-mar-09 N/A by model
LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02
LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-
009 MITSUBISHI SB 231 Rev B NYGE TDM01-45
02-apr-01 23-nov-01 Ref AMOC LFV Appr M15/01, TDM 01-45
LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02
LFV LVD 3166 Sprickkontroll av infästning till ving-spetstank
JCAB AD TCD-5747-2001 MITSUBISHI SB 236
20-sep-01 08-Oct-2001
LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-012 MITSUBISHI SB 237
09-jan-02 17-jan-02
LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB 239
21-mar-03 09-Oct-2003
MAI, Mitsubishi
Aircraft
International
MAI SB 047/30-001 A Torque of Bleed Air Tube Coupling
Nuts AD 84-12-04,SB 196A
FAA, U.S AD 84-12-04 MITSUBISHI SB 196
Rev A
19-jul-84 A 19-jun-84
MAI SB 051/27-007 Add.Seal and Flap Flexible Shaft
Torque AD 87-04-03, SB 198
FAA, U.S AD 87-04-03 01-feb-85 27-jan-83
MAI SB 067/27-008 A Insp/Repl. of Flap Control System
Torque AD 88-23-01, SB 189B
FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 03-mar-95
MAI SB 069/24-006 Split Radio Bus Inspection and
Rework
MAI SB 066/22-006 Rev A 17-nov-88 01-sep-89 N/A N/A due to Aircraft s/n
MAI SB 086/74-002 A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2435/97 MITSUBISHI SB 226 Rev E
05-Oct-2000
A 22-nov-01 Action not required due to s/n.
MAI SB 089/57-002 A Insp/Repl. of Bolts for Wing Tip Tank
FAA, U.S AD 98-20-39 05-nov-96 A 30-jan-97 N/A N/A due to s/n.
MAI SN 110/00-017A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MAI SN 111/77-004 Torque Indicating System Shift Potential
20-nov-08 11-mar-09 SB 233 considered
MAI SR 020/34-005 Anti Ice Capability AD 86-20-01, SR
053A
FAA, U.S AD 86-20-01 LFV LVD2015 Rev B
MITSUBISHI SR 053A
06-Oct-
1986
21-jan-00 N/A N/A due to s/n.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
139(195)
MITSUBISHI, Mitsubishi Heavy Industries Ltd
MITSUBISHI MSB 24-004
**RECOVERED RECORD** 27-jan-83 N/A
MITSUBISHI MSR 020
**RECOVERED RECORD** 12-jun-87
MITSUBISHI MSR
066
B **RECOVERED RECORD** 12-jun-87 B
MITSUBISHI SB 066 Bendix M4D 18-dec-87 18-May-
1988
N/A
MITSUBISHI SB
076/22-008
M-4() Autop.Engage Switch Guard
Install.
11-apr-91 12-apr-95 N/A
MITSUBISHI SB 112 C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-
1971
C 17-apr-86
MITSUBISHI SB 114 Fuel Quantity Indicator
Readjustmnet
JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.
MITSUBISHI SB 119 The Bolt and Bolt Hole Diam. of
Nose L.G
JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model
MITSUBISHI SB 123 Bearing,Oleo Strut,Nose L.G. -Repl. of
JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n
MITSUBISHI SB 124 Scissors Switch,Nose L.G. -Install. of 31-aug-70 17-apr-86 N/A
MITSUBISHI SB 128 B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n
MITSUBISHI SB 143 B Top Coating, Wing Integral Main
F.T.-SIo
JCAB AD TCD-0730-1-72 JCAB AD TCD-
0730-2-86
05-jan-72 B 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 162 A Flex. Shafts, Flap Control Sys.-Insp.
of (AD750201)
JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-
1974
A 21-aug-86 N/A
MITSUBISHI SB 163 B Insp. of Outer Pane, Front Winds. &
Inst
FAA, U.S AD 74-11-01 JCAB AD TCD-
0948A-1-78 JCAB AD TCD-0948A-74 LFV
LVA829 Rev A
16-nov-78 15-mar-86
MITSUBISHI SB 165 A Lubr. Interval,Wheel Bearing,Main
& Nose
24-jul-80 17-jun-86 N/A
MITSUBISHI SB 166 Wing Flap 24-jul-80 10-mar-86
MITSUBISHI SB 167 D Flap M.Jack Screw-Insp. of and/or Main G
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 LFV LVA1011 Rev A
24-jul-80 D 03-May-1977
Revision C PCW by Swedair.
MITSUBISHI SB 168 A Propeller Pitch Control Lever-Insp.
of (AD761620)
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-
75 LFV LVA1012
24-jul-80 A 25-apr-75
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2012-12-06
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MITSUBISHI SB 169 B Shimmy Damper-Insp. and
Modification of
JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW
MITSUBISHI SB 170 A MLG Forward Door Em.Op. Cable-
Insp. & Re (AD762204)
JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 17-apr-86 N/A N/A due to s/n
MITSUBISHI SB 171 B Latches,Eng. Nacelle Upper D.-
Insp.& Mod (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 LFV LVA1014 Rev A
17-nov-77 B 11-aug-78
MITSUBISHI SB 173 A Drag Strut, Main L.G.-Modification of
JCAB AD TCD-1284-1-76 24-jul-80 11-aug-75
MITSUBISHI SB 174
PART 1
C Tip Tank Conduit Tube-Insp.of,and
Rew.of (AD830902)
FINNISH AD M 1177/83 JCAB AD TCD-
1370A-81 LFV LVA1196
02-Oct-
1981
C 09-sep-10
MITSUBISHI SB 175 Barrel Nut, Inner/Outer Wing
Conn.-Repl.
JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by p/n
MITSUBISHI SB 176 E Elevator Trim Tab Bracket-Repl. of
LVD1971, AD 84-25-02, SB 031/27-
005R1
FAA, U.S AD 84-25-02 FINNISH AD M
1080/82 JCAB AD TCD-1001A-76 JCAB AD
TCD-1001B-2-84 LFV LVD1971
26-sep-84 E 19-mar-86
MITSUBISHI SB 177 B Mod. of Engine Nacelle Tail Area
(AD810601)
JCAB AD TCD-1379-1-80 LFV LVA1197 Rev
A
11-sep-80 B 23-jun-77 Previously complied with
MITSUBISHI SB 179 Rodd Assem., Engine Nacelle Upper D.-R&M
27-May-1977
04-feb-86
MITSUBISHI SB 180 A Link, Engine Nacelle Upper D.-Repl. of (AD780305)
FAA, U.S AD 78-03-05, JCAB AD TCD-1202-75 , LFV LVA1014 Rev A
17-nov-77 A 29-mar-78
MITSUBISHI SB 181 PART 2
B Insp. and Repl. of Nose L.G. Strut Assem (AD801812)
FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 LFV LVA1546
08-apr-85 B 24-aug-84
MITSUBISHI SB 182 Add. of Ceiling Cover, Rear Bagg.
Comp.
JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n.
MITSUBISHI SB 184 Turnbuckle, Control Cables -Repl. of 04-apr-80 25-mar-82
MITSUBISHI SB 188 Down Lock Mech., Nose L.G.-Insp. of
JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 25-mar-82
MITSUBISHI SB 189 C Flap Control Torque Tube AD 88-23-01, SB 067/27-008
FINNISH AD M 2722/00 JCAB AD TCD-2252-1-87 JCAB AD TCD-2252-83 LFV
LVA1873 LFV LVD2202
28-jun-94 C 03-mar-95
MITSUBISHI SB 190 A Trav. Nut Repl. of L.G. Mech. Stop
Assem
28-jun-94 25-mar-82
MITSUBISHI SB 191 Engine El. Wire-Insp. and
Replacement of (AD820802)
JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 25-mar-82
MITSUBISHI SB 193 B Landing Gear Warning Horn Syst.Modif.
15-jun-94 B 04-dec-00 Rev A är utförd.
MITSUBISHI SB 194 Master Cauting Light Visibility-Impr. of
23-aug-82 27-jan-83
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MITSUBISHI SB 196 A Ret. of coupling nut on the bleed
air tu AD 84-12-04, SB 047/30-001
FAA, U.S AD 84-12-04 JCAB AD TCD-2342-
1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A
12-apr-84 A 19-jun-84
MITSUBISHI SB 198 Add. Seal & Torque Insp. of Flap Flex.Sh LVD2037, AD 87-04-03, SB 051/27-007
FAA, U.S AD 87-04-03 JCAB AD TCD-2451-85 LFV LVD2037
13-feb-85 27-jan-83
MITSUBISHI SB 199 A Engine Lubricating Tubing Insp. & Protec
24-jun-94 A 06-nov-09 PCW
MITSUBISHI SB 200 B Insp of Nose Ldg Gear Drag Strut Link
24-jun-94 A 02-aug-88
MITSUBISHI SB 201 A Generator Circuit Wires Insp. and Mod.
FAA, U.S AD 87-12-02 JCAB AD TCD-2545-1-88 LFV LVD2191
02-mar-88 A 02-Oct-1986
MITSUBISHI SB 204 Speed Placard Change 03-mar-87 18-May-1988
MITSUBISHI SB 206 Bendix Autop.Disengagement Method Stand.
FAA, U.S AD 88-13-01 JCAB AD TCD-2856-1-97 LFV LVD2190
13-Oct-1987
31-jan-89 N/A N/A due to Autopilot model
MITSUBISHI SB 207 Rudder T.T. & Elevator T.T. Insp. & Rep.
20-May-1988
28-aug-09
MITSUBISHI SB 209 B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model
MITSUBISHI SB 210 A Engine Ignition Unit Replacement 12-nov-96 06-mar-98
MITSUBISHI SB 211 Rudder Trim Tab Modification (LVD 2338)
JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 212 A Insp of Anti-ice/Deice Systems (LVD 2347),
JCAB AD TCD-3393A-96 LFV LVD2347 Rev 1
25-apr-96 A 15-sep-10
MITSUBISHI SB 214 Engine Control Rod Inspection 06-dec-91 13-mar-92
MITSUBISHI SB 215 Removel of Prop. Governor Speed
Signal
23-Oct-
1991
13-mar-92 N/A N/A due to -1 engine
MITSUBISHI SB 216 Elevator Trim Tab Installation (LVD 2450
FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV
LVD2450 LFV LVD2537 LFV LVD2898
11-sep-92 26-May-1993
MITSUBISHI SB 218 A Propeller Feathering Linkage
Inspection
17-jan-94 A 15-mar-94
MITSUBISHI SB 219 A Emergency Gear Down G.box
Lower Pin Repl
JCAB AD TCD-3942-1-94 JCAB AD TCD-
3942-94 LFV LVD2538 LFV LVD2592
24-Oct-
1994
A 03-mar-95
MITSUBISHI SB 221 Tip Tank Conduit Tube Insp. and
Rep.
JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 15-mar-94
MITSUBISHI SB 222 Fuselage Waterproof Modification
SR 019
28-jun-94 08-dec-98
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2012-12-06
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142(195)
MITSUBISHI SB 223 Pitot/Static System Improvement
SR 064
MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 21-jan-00
MITSUBISHI SB 224 C Acrylic Windsheild/Window glass
Insp. UHB
FAA, U.S AD 2003-17-04 FINNISH AD M
3076 JCAB AD TCD-4311-95 LFV LVD2678
30-apr-98 C 09-sep-10
MITSUBISHI SB 225 Forward fitting bult of wingtip tank
LVD 2688
FAA, U.S AD 98-20-39 FINNISH AD M
2351/96 JCAB AD TCD-4310-96 LFV LVD2688
29-sep-95 30-jan-97
MITSUBISHI SB 226 E Auto-Ignition System Installation
LVD 2761 (2113), AD TCD-2679A-97
FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S
AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD-
2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A
18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n.
MITSUBISHI SB 227 Rudder Torque Tube Modification 20-dec-96 21-apr-98
MITSUBISHI SB 228 Elevator Trim Indicator Modification LFV 2898
FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 , LFV LVD2898
13-jul-98 08-dec-98
MITSUBISHI SB 229 Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689
20-feb-96 30-jul-96
MITSUBISHI SB 230 Mod.of Bearing Box Ldg. Gear Act. LVD 2819
JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 21-apr-98
MITSUBISHI SB 231 B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD
M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV
LVD3122 MAI SB 093/22-009 NYGE
TDM01-45
11-dec-02 B 03-mar-03 SL079 performed earlier.
MITSUBISHI SB 232 A De-Ice System Modification LVD
2800, TCD-4626-97
FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD
M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004
06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev 0.
MITSUBISHI SB 233 B Insp.of Engine Torque Indication System. TCD-4889-98, LFV 2924
FAA, U.S AD 2006-17-01 FINNISH AD M 2608/98 JCAB AD TCD-4889-2-2007 JCAB
AD TCD-4889-98 LFV LVD2924
08-mar-07 B 18-apr-07 Checked, previously carried out
MITSUBISHI SB 234 Fl.Check of the Flight Idle Fuel Flow
Se TCD-4890-98, LVD 2925
FAA, U.S AD 2006-17-05 JCAB AD TCD-
4890-98 LFV LVD2925
07-Oct-
1998
13-Oct-
2010
MITSUBISHI SB 235 Inspection of landing gear power train
JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model
MITSUBISHI SB 236 Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 08-Oct-2001
MITSUBISHI SB 237 Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02
MITSUBISHI SB 238 Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.
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2012-12-06
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143(195)
MITSUBISHI SB 239 Pneumatic Line Insp. and
Modification
JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 09-Oct-
2003
MITSUBISHI SB 240 Inst.of Trottle Quadrant Placard 26-feb-03 09-Oct-
2003
MITSUBISHI SB 241 A Inspection of Wing Attachment
Hardware
FAA, U.S AD 2006-13-15 JCAB AD TCD-
7030-2006
21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie
MITSUBISHI SL 060 System 17-feb-89 16-Oct-1991
MITSUBISHI SL 078 Automatic Autopilot Disconnect
System
28-jan-02 09-sep-10
MITSUBISHI SL 079 Diode inst.in Flap Position
Ind.Curcuit
28-jan-02 23-nov-01
MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt
Insp.
HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.
MITSUBISHI SL 084 Pneumatic De-Ice Monitoring
System
14-jun-04 09-sep-10
MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-
2005
17-sep-08 L/H side
MITSUBISHI SN 053 B Rudder Torque Tube AD 86-20-01,
SB 020/34-005
05-nov-86 B 30-jun-87
MITSUBISHI SN 117 D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD
TCD-4753-98 LFV LVD2922
14-jun-04 D 17-May-
2004
MITSUBISHI SN 146 Water Ingress into Vertical
Stabilizer
19-dec-03 26-apr-04
MITSUBISHI SN 148 Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB
MITSUBISHI SN 156A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MITSUBISHI SN 157 Torque Indicating System Shift Potential
20-nov-08 11-mar-09 SB 233 considered
MITSUBISHI SN 161 Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE
MITSUBISHI SN 164 part 2
IR Part 2, one time inspection of mechanical stop bearing
25-Jun-12
MITSUBISHI SR 053A
Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-2450A-87 LFV LVD2015 Rev B MAI SR 020/34-005 MITSUBISHI SB 223
23-Oct-1984
06-Oct-1986
MITSUBISHI SR 064 Pitot & Static System MITSUBISHI SB 223 30-apr-85 21-jan-00
MITSUBISHI SR 065 Warning Horn 20-jan-86 06-May-1988
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2012-12-06
Document number Page
144(195)
MITSUBISHI SR 067 Emergency Exit Placard 17-sep-85 15-apr-86
MITSUBISHI SR 072 Air Filter Replacement for Vacuum
Syst.
25-apr-00 29-apr-04
MITSUBISHI SR 075 Inst. tip tank placard 29-Oct-
2004
06-apr-05
MITSUBISHI STC
SA01913SE
Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-09 11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection
NARCO, Narco
NARCO SB ELT10-16 ELT ASSY 18-apr-88 16-Oct-1991
N/A
NYGE, Saab Aerotech
Aircraft Services
NYGE TDM 00-20 Fågelkollisionskada 07-Dec-
2000
11-dec-00
NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 06-jul-00
NYGE TDM 01-45 Installation of Trim-In-Motion Alert Syst. and Automatic A/P Disconnect syst.
JCAB AD TCD-4625A-2001 LFV LVD3122 MITSUBISHI SB 231 Rev B
07-May-2001
23-nov-01
NYGE TDM 01-61 Installation Ceis ELT 10-dec-01 08-jan-02
NYGE TDM 02-10 Installation of TPE331-6-252M
Engines
25-mar-02 29-apr-04
NYGE TDM 02-24 Installation Moving MAP 10-Oct-2002
31-Oct-2002
NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04
NYGE TDM 02-33 Viktminskning MU-2B 24-dec-02 09-aug-01
NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330
install.
04-mar-03 31-Oct-
2008
NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 04-mar-03 Original compliance was as per TDM rev A.The A/C
installation is IAW rev C as not affected by rev B and C.F01324, F01341, F01342
NYGE TDM 03-15 A U95 with General Control System 24-apr-03 A 25-feb-08
NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 30-aug-05 Original compliance with previous revision not affected by rev F.F01211, M03323,R01395
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2012-12-06
Document number Page
145(195)
NYGE TDM 05-03 Marcus "Installation" 16-feb-05 02-feb-06
NYGE TDM 05-04 ADL Installation 16-feb-05
NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05
NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 29-nov-07
NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06 A 07-feb-08
NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07 A 07-feb-08
NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 28-feb-08
NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 28-aug-09
NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 31-Oct-2008
Original compliance with TDM rev A. Rev B does not affect previous complaiance.
NYGE TDM 09-29 A GPS Splitter 12-Oct-2009
A 10-feb-10
NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May-
2010
C/W
NYGE TDM 11-16 19" instrumentrack 04-Oct-
2012
NYGE TDM 11-35 A Terminating resistor 27-Jan-12
NYGE TDM 12-21 A Avinstallation IK 29-Jun-12
NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 26-apr-04
NYGE TDM 97-03 Astor MU-2 25-feb-97 23-apr-97
NYGE TDM 98-08 Torrluft ASTOR 27-May-
1998
23-jul-98
NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 15-jun-99
NYGE TVO 1/09 Inspektion av Stringers & struktur vinge
25-feb-09 08-apr-09 Inspected with remarks
NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 26-May-1993
NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 26-jun-00
NYGE TVO 1/97 3 De-Icertank MU-2B,
korrosionskontroll
12-feb-97 14-May-
1997
NYGE TVO 2/00 Märkning av infästning domkraft Mu2
01-dec-00 04-apr-01
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2012-12-06
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NYGE TVO 2/07 A Prevent FR31 radio to xmit when
RM2 off
06-feb-07 A 02-mar-07
NYGE TVO 2/91 A/C Elecrical System 10-jan-91 13-mar-92
NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06 09-sep-10
NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 28-aug-09
NYGE TVO 4/11 Static inverter controll A 15-Dec-11
NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 09-sep-10
NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 16-Oct-1991
NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 14-Oct-1992
NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 09-sep-10 R/H
NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning.
25-Oct-1996
20-mar-97
NYGE TVO 4/99 Kontroll av rullbälten 09-apr-99 15-apr-99
NYGE TVO 6/88 Allm. instruktion för
metallpropeller
13-jun-88 15-sep-08
NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-1992
20-nov-92
NYGE TVO 7/93 Starter Drive Splines 01-nov-93 15-mar-94
NYGE TVO 8/04 Kontr. av Spant vid bakre
feninfästning
08-dec-04 09-sep-10
NYGE TVO 8/92 Wheel Parts 27-Oct-
1992
02-apr-93
NYGE TVO 9/88 Emergency Extension System 08-aug-88 03-nov-88
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2012-12-06
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2.6 GFE Aircraft Mitsubishi MU-2 SE-IOV
2.6.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
MU-2B-26 337 SE-IOV 11473 4130 2012-11-23
2.6.2 Engines Type: Honeywell TPE331-6-252M
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours remaining
overhaul/HSI/GBI:
Left Engine P20067 11697 10203 1598/1428/3228
Right Engine P20376 10279 10813 2884/1161/1084
2.6.3 Propeller Type Number: Serial Number: Overhaul Due Date:
Left Propeller HC-B3TN-5E BUA 19597 2013-11-25
Right Propeller HC-B3TN-5E BVA 6186 2013-01-07
2.6.4 Avionics System: Type / Part Number: Note:
Autopilot & Flight Director Bendix M4D
COM/NAV/GPS 1 & 2 Garmin GNS 430
Audiopanel Bendix/King KMA-24H-70
MKR Bendix/King KMR 675
DME Bendix/King KN 63
ADF Bendix/King KR 87
XPDR 1 Garmin GTX 330D
XPDR 2 Garmin GTX 330 *)
RDR ALT Bendix/King KRA-10A
ELT Kanad ELT 406-AF-H
Airspeed Indicator LH / RH Aerosonic 30040-0186 / 30040-
0186
Altimeter LH United Instr. Inc. 5934 PAM-3
Altimeter incl. encoder RH United Instr. Inc. 5035P-P40
Altitude Reporter Ameri-King AK-350
Altitude Alerter Century 1D960
Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3
Attitude Gyro & Flight Director Ind. Bendix GH-14
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2012-12-06
Document number Page
148(195)
LH
Attitude Gyro Ind. RH AIM 504-0006-914
Turn & Bank Ind. LH Bendix 4099-B
Horizontal Situation Indicator LH Bendix RD-44
DG-Gyro Sperry C-14A
RMI Indicator Collins 332C-10
RMI/ADF adapter Bendix/King KDA-692
CDI Indicator Garmin GI-106A
*) XPDR 2 without diversity configuration
2.6.5 Mission System System: Description:
Fixed general installations
VHF/UHF COM FR31
GPS MAP
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
Laser Prism
MIL-STD-1553 Bus LH Wing Pylon
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ADRIAN Pod mounted system LH and RH Wing
Pylon
U95 Sorc Pod mounted system RH Wing Pylon
A100 Pod mounted system LH Wing Pylon
Missile Threat Simulator
DARTS Pod mounted system LH Wing Pylon
Chaff Dispenser
BOX 3 Pod mounted system LH and RH Wing
Pylon
Target Towing
MBV7S Inboard winch
AS200 MDI (Miss Distance Indicator)
Precisions GPS Pos System
TAPS
Radar Calibration System
GPS Sphere
2.6.6 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, U95 Sorc,
A100, DARTS and BOX 3 General Signal Harness AWG22 shielded x 44
General Signal Harness AWG22 shielded x 50
U95-Sorc and A100 MIL-STD-1553B Data Triax Cable x 1
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2012-12-06
Document number Page
149(195)
Bus U95 Sorc, A100 and DARTS AC Power
115/200VAC 400 Hz 3-
Phase 3 x 10 A
AWG 16 x 4
twisted
AWG 16 x 2
AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200
A
DC Power 28 VDC 200
A
AWG 2 x 2
Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω
U95 Sorc Ethernet LAN Cable
2.6.7 Antenna Layout
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2012-12-06
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2.6.8 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date
Aircraft SE-IOV
Vingstudie MU-2 AMP 2010-10-08 11219 12250
100 Hour Inspection AMP 2012-03-01 11399 11499 2013-03-01
200 Hour Inspection AMP 2012-03-01 11399 11599 2013-03-20
600 Hour Inspection AMP 2011-01-31 11230 11830,1 2014-02-17
1000 Hour Inspection AMP 2011-01-19 1230 12250
1200 Hour Inspection AMP 2008-01-14 10835 12035
1800 Hour Inspection AMP 2005-01-03 10250 12050
2000 Hour Inspection AMP 2005-01-03 9650 11650
1 Year Inspection AMP 2012-03-02 11399 2013-03-20
2 Year Inspection AMP 2012-01-24 11384 2014-01-25
10 Year Inspection AMP 2005-01-04 10250 2015-01-02
Engine S/N P-20067 Remaining
Engine Assembly (Overhaul) AMP 13072 1598,7
Engine Hot Section Inspection AMP 12901,9 1428,6
Engine Gearbox Inspection AMP 14701,9 3228,6
Engine S/N P-20376
Engine Assembly (Overhaul) AMP 14357,5 2884,2
Engine Hot Section Inspection AMP 12634,7 1161,4
Engine Gearbox Inspection AMP 12557,5 1084,2
Propeller L/H O/H AMP 2008-11-26 14361,5 2013-11-25
Propeller R/H O/H AMP 2008-01-09 13834,7 2013-01-07
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
151(195)
2.6.9 Implemented Changes Status date November 23
rd 2012.
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Compliance Stat
us
Remarks
EASA, European Aviation
Safety Agency
EASA AD 2006-0265
Incorrect transponder altitude 30-aug-06 11-feb-10
EASA AD 2009-
0251-E
Portable Fire Extinguishers-Ident/Repl 25-nov-09 07-May-2010 N/A N/A by current P/N installed
EASA AD 2009-
0262
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-2010 N/A N/A by current P/N installed
EASA AD 2009-
0278
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09 07-May-2010 N/A N/A by current P/N installed
EASA AD 2010-
0003
R1 Mode S Transponder -
Check/Modification
11-jan-10 R1 10-mar-10 N/A due to model
EASA AD 2012-
0037
KIDDE GRAVINER HAND OPERATTED
FIRE EXTINGUISHER
06-Sep-12
EASA SIB 2008-58R1
Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN SSB0845 Rev IR
17-dec-08 21-sep-10 N/A by SSB 0844 incorporated
EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model
FAA, U.S, Federal Aviation Administration
FAA, U.S AD 2000-
02-25
AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b.
FAA, U.S AD 2000-
09-15
1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M
2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004
MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A
07-jul-00 22-nov-01 Action not required due to s/n.
FAA, U.S AD 2003-17-04
Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 087/56-001 Rev B MITSUBISHI SB 224 Rev C
01-Oct-2003
08-mar-11
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
152(195)
FAA, U.S AD 2003-
22-07
1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-
4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D
16-apr-04 17-May-2004 inserted in AFM limitations
FAA, U.S AD 2005-14-12
Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 20-sep-05
FAA, U.S AD 2005-18-20
Prop de-icer "FASTprop" 14-Oct-2005
12-Oct-2005 N/A Due to boots p/n
FAA, U.S AD 2006-
13-15
Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB
241 Rev A
11-aug-06 23-feb-04 c/o in conjunction with vingstudie
FAA, U.S AD 2006-
15-07
Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229
FAA, U.S AD 2006-
17-01
Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233
Rev B
22-sep-06 21-sep-06 PCW see MSB 233A
FAA, U.S AD 2006-
17-05
Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 11-feb-10
FAA, U.S AD 2007-
17-09
Reduce max deflect elev nose-down
trim
MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's.
FAA, U.S AD 71-14-01
Fuel Tank Fungus Coating Peeling 01-May-1972
01-jan-96 N/A N/A by s/n
FAA, U.S AD 75-03-06
Cracks and Optical Distortion LFV LVA829 Rev A 13-nov-74 21-aug-85 N/A N/A due to s/n.
FAA, U.S AD 75-16-13
Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev A MITSUBISHI SB 167 Rev D
05-aug-75 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
FAA, U.S AD 75-
16-20
Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012
MITSUBISHI SB 168 Rev A
12-aug-75 21-aug-85
FAA, U.S AD 78-
03-05
Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A
MITSUBISHI SB 171 Rev B MITSUBISHI SB
180 Rev A
23-feb-78 21-aug-85
FAA, U.S AD 81-06-01
1 Engine Aft Nacelles 01-apr-81 1 27-jan-86 Previously complied with
FAA, U.S AD 82-08-02
Electrical Wiring Inspection 15-apr-82 27-aug-87
FAA, U.S AD 83-08-01
2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD T5114/05 HARTZELL SI 140A Rev 9
28-apr-82 2 20-May-2005 Ref. MU2B MM chap 13.4 when using bolts P/N B-3339 only
FAA, U.S AD 84-12-04
Torque of Air Tube Coupling Nuts SB 047/30-001, SB 196A
MAI SB 047/30-001 Rev A MITSUBISHI SB 196 Rev A
28-jun-84 27-jan-86
FAA, U.S AD 84-25-02
Elevator TrimTab Bracket Insp/Repl. SB 031/27-005 R1, SB 176E
MAI SB 031/27-005 Rev 1 MITSUBISHI SB 176 Rev E
18-dec-84 21-aug-85
FAA, U.S AD 86-
15-03
NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2
Rev B
13-aug-86 15-jul-04 Found SB 181 part 2 PCW.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
153(195)
FAA, U.S AD 86-
20-01
To assure anti-ice capability of pitot
SB 020/34-005, SB 053A
LFV LVD2015 Rev B MAI SR 020/34-005
MITSUBISHI SR 053A
06-Oct-
1986
27-mar-00
FAA, U.S AD 86-
26-02
To prevent engine flameout in an
iceing SB 74-0003, SR 040/74-001
GARRETT SB 74-0003 Rev 6 31-dec-87 09-mar-09 see applicable engine for c/o
FAA, U.S AD 87-
04-03
Addit. Seal and Flap Flexible Shaft
Insp SB 051/27-007, SB 198
MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 27-aug-84
FAA, U.S AD 87-12-02
Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 27-mar-09 N/A by s/n
FAA, U.S AD 88-
13-01
Bendix Autopilot Disengagement SB
066/22-006
LFV LVD2190 MAI SB 066/22-006 Rev A
MITSUBISHI SB 206
11-jul-98 25-jul-89
FAA, U.S AD 88-
21-01
1 To minimize confusion in
autopilot/manua SB 066/22-006
LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-12
FAA, U.S AD 88-
23-01
To prevent flap control failure SB
067/27-008, SB 189B
LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 11-mar-96
FAA, U.S AD 93-
07-11
ELECTRIC TRIM SYSTEM SB 079/27-
010
LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n
FAA, U.S AD 94-
04-16
Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 07-May-1993
FAA, U.S AD 94-
11-04
Change of Flight Idle Blade Angel SB
016/61-001
LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n
FAA, U.S AD 96-
18-14
Inspection / Replacement of Prop
Hub. LVD 2732, Hx SB 136G
FINNISH AD M 2404/96 Rev 1 HARTZELL
SB 61-261 Rev 1 LFV LVD2732
16-Oct-
1996
01-sep-99 Prop utbytt mot S/N BVA-series
FAA, U.S AD 96-
25-02
Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-
4552-96 LFV LVD2749
27-dec-96 11-mar-02
FAA, U.S AD 97-
04-13
Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-1997 N/A N/A due to model.
FAA, U.S AD 97-
20-14 CNL
Icing related incidents/accidents 17-Oct-
1997
02-dec-98
FAA, U.S AD 97-
25-02
To prevent loss of airplane
ctrl/overspe
FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17
FAA, U.S AD 98-
20-39
Forward fitting bolt of wingtip tank SB
MU-2 225, 089/57-002A
LFV LVD2688 , MITSUBISHI SB 225 19-Oct-
1998
04-dec-96
FINNISH, Finnish Civil
Aviation Adm
FINNISH AD M
3076
Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 , MAI SB
087/56-001 Rev B , MITSUBISHI SB 224 Rev C
21-aug-03 08-mar-11
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
154(195)
GARMIN, Garmin
GARMIN SB 0004 Incorp.of Main Software Version 2.16 01-May-2000
18-May-2000
GARMIN SSB 0844
IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 24-May-2010
GARRETT,
AlliedSignal
Aerospace
GARRETT SB 74-
0003
6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 09-mar-09 see applicable engine for c/o
HARTZELL,
Hartzell Propeller
Inc.
HARTZELL SB 61-
256
Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI
SL 080
08-feb-02 24-apr-02 R/H side
HARTZELL SB 61-
279 ALERT
4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL
085
04-Oct-
2005
14-nov-05 propellerbolts previously checked u/a
HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV
LVA1424 Rev A
30-mar-05 9 13-mar-08 see previously revision
JCAB, Japan Civil
Aviation Bureau
JCAB AD TCD-
0518-68
Rivet holes elevator hinge fitting 06-feb-68 26-mar-09 N/A by s/n
JCAB AD TCD-
0642-70
AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 21-aug-85 N/A by s/n
JCAB AD TCD-0643-70
Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A N/A by s/n.
JCAB AD TCD-0652-70
Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-0653-70
Engine Nacelle Tail Area-Modification of 25-mar-70 26-mar-09 N/A by model
JCAB AD TCD-0660-70
Replacement of bearing in nosegearstrut
LFV LVA457 MITSUBISHI SB 123 01-May-1970
26-mar-09 N/A by s/n
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
155(195)
JCAB AD TCD-
0730-1-72
Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143
Rev B
25-mar-72 14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
0730-2-86
Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n
JCAB AD TCD-
0859-72
Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to model.
JCAB AD TCD-0866-72
NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-1972
31-dec-72 N/A N/A due to model.
JCAB AD TCD-
0947A-74
Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162
Rev A
12-nov-74 27-jan-86 N/A N/A due to s/n.
JCAB AD TCD-
0948A-1-78
Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09 N/A by s/n
JCAB AD TCD-
0948A-74
Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163
Rev B
07-Oct-
1974
21-aug-85 N/A N/A due to s/n.
JCAB AD TCD-
1001A-76
Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176
Rev E
06-Oct-
1976
27-aug-84
JCAB AD TCD-
1001B-2-84
Replacement of Elevator Trim Tab
Bracket
FINNISH AD M 1080/82 LFV LVD1971
MITSUBISHI SB 176 Rev E
12-dec-84 21-aug-85
JCAB AD TCD-
1094A-76
Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev
A MITSUBISHI SB 167 Rev D
06-sep-76 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
JCAB AD TCD-
1188-75
Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012
MITSUBISHI SB 168 Rev A
06-May-
1975
21-aug-85
JCAB AD TCD-
1202-75
Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev
A MITSUBISHI SB 171 Rev B MITSUBISHI
SB 180 Rev A
20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW.
JCAB AD TCD-
1209-75
Insp/mod of NLG shimmydamper
locking
LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 27-jan-86
JCAB AD TCD-
1235-75
Insp./repl. of MLG fwd door
emerg.cables
LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 21-aug-85 N/A N/A due to model.
JCAB AD TCD-
1272-75
Supp.,MLG Forward D. Actuating
Mech.-I&M
MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model
JCAB AD TCD-
1284-1-76
Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 09-nov-09 PCW Carried out ref SB 173, date 1985/08/21
JCAB AD TCD-
1328-76
Fire hazard in rear baggage
compartment
01-jul-76 26-mar-09 N/A by s/n
JCAB AD TCD-
1353-76
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
MITSUBISHI SB 175 16-aug-76 26-mar-09
JCAB AD TCD-
1370-76
Inspect strobelight conduit in Tiptank LFV LVA1196 18-Oct-
1976
27-jan-86 N/A by s/n
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
156(195)
JCAB AD TCD-
1370A-81
Inspect strobelight conduit in Tiptank
supersed TCD-1370-76
MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 24-mar-09 N/A by s/n
JCAB AD TCD-
1379-1-80
Insp. rear eng. cowling reg. heatdamage LFV LVA1197 Rev A MITSUBISHI SB 177
Rev B
06-feb-02 27-jan-86
JCAB AD TCD-
1520A-77
Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180
JCAB AD TCD-1768-1-85
Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 2 Rev B
12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.
JCAB AD TCD-
1817-79
Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 27-May-1986 N/A N/A due to s/n.
JCAB AD TCD-
2048-81
Insp. firewarning & emerg.power circuit LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-1981 N/A N/A due to s/n.
JCAB AD TCD-
2070-81
Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 27-aug-84
JCAB AD TCD-
2113-82
Insp./replace engine electrical harness LFV LVA1788 MITSUBISHI SB 191 06-feb-02 27-aug-84
JCAB AD TCD-
2252-2-88
Flap system torquetubes supersed TCD-
2252-1-87
01-feb-89 24-mar-09 PCW
JCAB AD TCD-
2252-83
Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 11-mar-96
JCAB AD TCD-
2263-83
NLG. bracket attaching to drag strut 13-aug-83 24-mar-09 N/A by model
JCAB AD TCD-
2342-1-84
Engine inlet anti-ice tubing. Torq./lock MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW
JCAB AD TCD-
2342-84
Engine inlet anti-ice tubing. Torq./lock LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 27-jan-86
JCAB AD TCD-
2450A-87
Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.
JCAB AD TCD-
2451-1-87
Add. seal/Tq. insp of flap flex. shaft 01-May-
1987
09-mar-09 PCW see TCD-2451-85
JCAB AD TCD-
2451-85
Add. seal/Tq. insp of flap flex. shaft
Superseeded by TCD-2451-1-87
LFV LVD2037 MITSUBISHI SB 198 30-sep-85 27-aug-84
JCAB AD TCD-
2545-1-88
Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 24-mar-09 N/A by s/n
JCAB AD TCD-2679A-97
Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 01-feb-97 22-nov-01
JCAB AD TCD-2856-1-97
Bendix M4C Autopilot System MITSUBISHI SB 206 05-nov-97 06-nov-09 N/A Due to model
JCAB AD TCD-3378-90
Insp./mod. of rudder trimtab leadingedge
LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
157(195)
JCAB AD TCD-
3393A-96
Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347
Rev 1 MITSUBISHI SB 212 Rev A
25-May-
1996
11-feb-10
JCAB AD TCD-
3464-91
Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model
JCAB AD TCD-
3740A-98
Mod.of Autopilote pitchtrimsystem
MSB 216, 228 LVD 2898
FINNISH AD M 2581/98 LFV LVD2450
LFV LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228
17-aug-98 09-nov-98
JCAB AD TCD-
3901-93
Tiptank inst FINNISH AD M 2110/93 LFV LVD2512
MITSUBISHI SB 221
10-sep-93 25-apr-94
JCAB AD TCD-
3942-1-94
Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592
MITSUBISHI SB 219 Rev A
28-nov-94 27-mar-95
JCAB AD TCD-
3942-94
Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 27-mar-95
JCAB AD TCD-
4310-96
Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688
MITSUBISHI SB 225
01-apr-96 04-dec-96
JCAB AD TCD-
4311-95
Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678
MITSUBISHI SB 224 Rev C
01-nov-95 08-mar-11
JCAB AD TCD-4379-96
Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 MITSUBISHI SB 229
01-apr-96 30-jul-96
JCAB AD TCD-4552-96
Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 11-mar-02
JCAB AD TCD-4625-97
Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 093/22-009
14-jul-97 15-May-2001
JCAB AD TCD-
4625A-2001
Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B
NYGE TDM01-45
16-mar-01 13-mar-09 PCW
JCAB AD TCD-
4626-97
De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800
MITSUBISHI SB 232 Rev A
01-May-
1997
14-jul-04 PCW
JCAB AD TCD-
4684-97
Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819
MITSUBISHI SB 230
01-jun-97 25-mar-99
JCAB AD TCD-
4753-98
Ändring av flyghandbok LVD 2922,FAA
AD 97-20-14, MHI SN 117A
FINNISH AD M 2518/98 LFV LVD2922
MITSUBISHI SN 117 Rev D
18-feb-98 02-dec-98 FAA AD utförd.
JCAB AD TCD-
4753A-2004
Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-2004 inserted in AFM limitations
JCAB AD TCD-
4838-98
Inspection of landing gear power train FINNISH AD M 2574/98 LFV LVD2897
MITSUBISHI SB 235
04-aug-98 24-mar-09 N/A by model
JCAB AD TCD-
4889-2-2007
Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.
JCAB AD TCD-
4889-98
Insp. of Engine Torque Indication
System LFV 2924, MU SB 233
FINNISH AD M 2608/98 LFV LVD2924
MITSUBISHI SB 233 Rev B
05-nov-98 14-jul-04 PCW
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
158(195)
JCAB AD TCD-
4890-98
Check of flight idle FF LVD 2925, MU SB
234
FINNISH AD M 2609/98 LFV LVD2925
MITSUBISHI SB 234
04-nov-98 11-feb-10
JCAB AD TCD-
5030-99
Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-
1999
24-mar-09 N/A by model
JCAB AD TCD-
5432-2000
AFM revision LFV LVD3112 27-nov-00 12-feb-02
JCAB AD TCD-5547-2001
To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02
JCAB AD TCD-
5747-2001
Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 18-Oct-2001
JCAB AD TCD-
5864-2001
Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 17-jan-02
JCAB AD TCD-
6127-2003
Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 02-Oct-2003
JCAB AD TCD-
7030-2006
Inspection of Wing Attachment
Hardware
MITSUBISHI SB 241 Rev A 27-dec-06 17-jan-07 c/o in conjunction with wingstudie
LFV,
Luftfartsverket
LFV LVA 1011 A Kontroll av vingklaffarnas manöversystem
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 MITSUBISHI SB 167 Rev D
05-feb-02 A 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
LFV LVA 1012 Kontroll av propellerreglagets montering
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 MITSUBISHI SB 168 Rev A
05-feb-02 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 Rev B
05-feb-02 27-jan-86
LFV LVA 1014 A Kontr. & byte av motorinkl. låsanordning
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
05-feb-02 A 21-aug-85
LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A
05-feb-02 21-aug-85 N/A N/A due to s/n
LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174 PART 1 Rev C
06-feb-02 06-feb-02 N/A by s/n
LFV LVA 1197 A Förhindr. av värmeskador på bak.motorpl.
JCAB AD TCD-1379-1-80 MITSUBISHI SB 177 Rev B
06-feb-02 A 27-jan-86
LFV LVA 1238 Kontr. & byte av infästningsdet. trimrod 06-feb-02 21-apr-09 N/A by s/n
LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 MITSUBISHI SB 181 PART 2
Rev B
06-feb-02 27-May-1986
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2012-12-06
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159(195)
LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB
182
05-feb-02 11-feb-80 N/A N/A due to s/n.
LFV LVA 1740 Kontr.av brandvarnings-och
n"dstr"mskret
JCAB AD TCD-2048-81 MITSUBISHI SB
187 Rev B
05-feb-02 31-aug-09 N/A by s/n
LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB
188
05-feb-02 27-aug-84
LFV LVA 1788 Kontroll/Utbyte av elledningar på motor
JCAB AD TCD-2113-82 MITSUBISHI SB 191
06-feb-02 27-aug-84
LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB
189 Rev C
06-feb-02 11-mar-96
LFV LVA 1942 Momentdragning/låsn.av koppl.i
varmlufts
JCAB AD TCD-2342-84 MITSUBISHI SB
196 Rev A
06-feb-02 27-jan-86
LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB
114
05-feb-02 21-aug-85 N/A N/A by s/n
LFV LVA 439 Rev. av flyghandbok betr. bränslespec. JCAB AD TCD-0642-70 MITSUBISHI SB
112 Rev C
05-feb-02 21-aug-85 N/A by model
LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB
119
05-feb-02 26-mar-09 N/A by model
LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD-0660-70 MITSUBISHI SB
123
05-feb-02 26-mar-09 N/A by s/n
LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.
LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156
05-feb-02 08-dec-09 N/A by A/C serial number
LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n & model
LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB 162 Rev A
05-feb-02 A 27-jan-86 N/A N/A due to s/n.
LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-06 JCAB AD TCD-0948A-74
MITSUBISHI SB 163 Rev B
05-feb-02 A 21-aug-85 N/A N/A due to s/n.
LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 27-aug-84
LFV LVD 1238 Kontr./byte infästn.det. höjdtrimroder 15-apr-77 31-aug-09 N/A by s/n
LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI
SB 176 Rev E
18-jan-85 27-May-1986
LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005
Rev A, MHI SR 53
FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 MAI SR 020/34-005 MITSUBISHI SR 053A
24-May-
1985
B 21-aug-85
LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 30-sep-85 27-May-1986
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2012-12-06
Document number Page
160(195)
198
LFV LVD 2069 Altimeter 25-mar-86 27-May-1986 N/A N/A by p/n & s/n
LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA
26-jan-87 19-feb-87
LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006 och SB 206
FAA, U.S AD 88-13-01 MAI SB 066/22-006 Rev A MITSUBISHI SB 206
19-aug-88 25-jul-89
LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB
201 Rev A
19-aug-88 24-mar-09 N/A by s/n
LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-
2252-1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C
08-dec-88 11-mar-96
LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-Dec-1988
12-feb-02
LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB 211
JCAB AD TCD-3378-90 MITSUBISHI SB 211
28-mar-91 14-jul-04 N/A N/A by s/n.
LFV LVD 2347 1 Control Deice-system Mitsubishi SB 212A
JCAB AD TCD-3393A-96 MITSUBISHI SB 212 Rev A
29-May-1996
1 11-feb-10
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9
23-May-1991
14-jun-91 checked OK.
LFV LVD 2450 Elevator Trim Tab Installation MU SB
216
JCAB AD TCD-3740A-98 MITSUBISHI SB
216
03-dec-92 07-May-1993
LFV LVD 2477 Electric Trim System AD930711, MU SB
079/27-0-010
FAA, U.S AD 93-07-11 MAI SB 079/27-
010
03-jun-93 27-mar-09 N/A by s/n
LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB
221
02-dec-93 25-apr-94
LFV LVD 2537 Reducering av Höjdrodrets trimområde.
FAA AD 94-04-16, SB 216
FAA, U.S AD 94-04-16 MITSUBISHI SB
216
07-apr-94 07-May-1993
LFV LVD 2538 Byte Låspinne i landställets nödutf. SB
219
JCAB AD TCD-3942-94 MITSUBISHI SB
219 Rev A
07-apr-94 27-mar-95
LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n
LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox
TCD-3942-1-94, MSB 219A
JCAB AD TCD-3942-1-94 MITSUBISHI SB
219 Rev A
09-feb-95 27-mar-95
LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB
224 Rev A
FAA, U.S AD 2003-17-04 JCAB AD TCD-
4311-95 MITSUBISHI SB 224 Rev C
12-mar-96 08-mar-11
LFV LVD 2688 Kontr/byte av infästn.bult för tiptank MU-2 SB 225
FAA, U.S AD 98-20-39 JCAB AD TCD-4310-96 MITSUBISHI SB 225
09-May-1996
04-dec-96
LFV LVD 2689 Kontroll av linkage för prop.flöjning MU-2 SB 229
JCAB AD TCD-4379-96 MITSUBISHI SB 229
09-May-1996
30-jul-96
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2012-12-06
Document number Page
161(195)
LFV LVD 2732 Inspection/ Replacement of Prop Hub.
FAA AD 96-18-14, Hz SB 136H
FAA, U.S AD 96-18-14 HARTZELL SB 61-
261 Rev 1
27-sep-96 01-sep-99 Prop. utbytt mot BVA
LFV LVD 2749 Revision av flyghandbok AFM TCD-
4552-96
FAA, U.S AD 96-25-02 JCAB AD TCD-
4552-96
21-jan-97 11-mar-02
LFV LVD 2761 Installation av autoignition system TCD-
2679A-97
JCAB AD TCD-2679A-97 MITSUBISHI SB
226 Rev E
14-feb-97 05-mar-99
LFV LVD 2769 Demont.av backventil i bränslesystemets MU-2 SB 130A
FAA, U.S AD 97-04-13 MITSUBISHI SB 130 Rev A
18-mar-97 05-May-1997 N/A N/A due to s/n.
LFV LVD 2800 Mod. av De-ice Monitoring System
Mitsubishi SB 232, TCD-4626-97
JCAB AD TCD-4626-97 MITSUBISHI SB
232 Rev A
28-aug-97 10-May-1998
LFV LVD 2819 Mod.av lagerboxar för landställssystem
Mitsubishi SB 230
JCAB AD TCD-4684-97 MITSUBISHI SB
230
18-nov-97 18-mar-98
LFV LVD 2897 Kontroll av landst,llets drivsystem TCD-
4838-98, SB 235
JCAB AD TCD-4838-98 MITSUBISHI SB
235
02-aug-98 24-mar-09 N/A by model
LFV LVD 2898 Mod. av autopilotens höjdtrimsystem
TCD-3740A-98, SB 216, 228
JCAB AD TCD-3740A-98 MITSUBISHI SB
216 MITSUBISHI SB 228
27-aug-98 09-nov-98
LFV LVD 2922 Änd.av Flyghandbok-Extra krav på
typutbi TCD-4753-98, MHI SN 117A
JCAB AD TCD-4753-98 MITSUBISHI SN
117 Rev D
12-nov-98 02-dec-98 FAA AD utförd.
LFV LVD 2924 Kontr/Just av motorernas Torque
indikeri MHI SB 233, TCD-4889-98
JCAB AD TCD-4889-98 MITSUBISHI SB
233 Rev B
01-dec-98 03-jun-99
LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id
MHI SB 234
JCAB AD TCD-4890-98 MITSUBISHI SB
234
01-dec-98 20-apr-99
LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB
209 Rev B
18-jun-99 24-mar-09 N/A by model
LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02
LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-009 MITSUBISHI SB 231 Rev B NYGE TDM01-45
02-apr-01 15-May-2001
LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02
LFV LVD 3166 Sprickkontroll av infästning till ving-spetstank
JCAB AD TCD-5747-2001 MITSUBISHI SB 236
20-sep-01 18-Oct-2001
LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-012 MITSUBISHI SB 237
09-jan-02 17-jan-02
LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB 239
21-mar-03 02-Oct-2003
MAI, Mitsubishi
Aircraft
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2012-12-06
Document number Page
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International
MAI SB 047/30-
001
A Torque of Bleed Air Tube Coupling Nuts
AD 84-12-04,SB 196A
FAA, U.S AD 84-12-04 MITSUBISHI SB
196 Rev A
19-jul-84 A 27-jan-86
MAI SB 051/27-
007
Add.Seal and Flap Flexible Shaft Torque
AD 87-04-03, SB 198
FAA, U.S AD 87-04-03 01-feb-85 27-aug-84
MAI SB 066/22-
006
Bendix autopilot disengagement 21-Mar-12
MAI SB 067/27-
008
A Insp/Repl. of Flap Control System
Torque AD 88-23-01, SB 189B
FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 11-mar-96
MAI SB 069/24-
006
Split Radio Bus Inspection and Rework MAI SB 066/22-006 Rev A 17-nov-88 25-jul-89 N/A N/A due to Aircraft s/n
MAI SB 086/74-002
A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2435/97 MITSUBISHI SB 226 Rev E
05-Oct-2000
A 22-nov-01 Action not required due to s/n.
MAI SB 089/57-002
A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 04-dec-96 N/A N/A due to s/n.
MAI SN 110/00-017A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MAI SN 111/77-004
Torque Indicating System Shift Potential 20-nov-08 11-mar-09 SB 233 considered
MAI SR 020/34-005
Anti Ice Capability AD 86-20-01, SR 053A
FAA, U.S AD 86-20-01 LFV LVD2015 Rev B MITSUBISHI SR 053A
06-Oct-1986
27-mar-00 N/A N/A due to s/n.
MITSUBISHI,
Mitsubishi Heavy
Industries Ltd
MITSUBISHI MSB
24-002
A **RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB
24-004
**RECOVERED RECORD** 17-Oct-
1984
N/A
MITSUBISHI MSB 27-001
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 27-003
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 27-005
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 27-006
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB **RECOVERED RECORD** 27-aug-84 N/A
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
163(195)
27-007
MITSUBISHI MSB
30-001
A **RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB
32-001
A **RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB
32-004
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB
32-006
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB
32-010
**RECOVERED RECORD** 07-jul-86 N/A
MITSUBISHI MSB 34-004
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 34-007
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 54-001
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 54-002
A **RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 71-003
B **RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSB 71-005
**RECOVERED RECORD** 27-aug-84 N/A
MITSUBISHI MSR 066
B **RECOVERED RECORD** 19-feb-87
MITSUBISHI SB 066
Bendix M4D 18-dec-87 25-jul-89
MITSUBISHI SB 076/22-008
M-4() Autop.Engage Switch Guard Install.
11-apr-91 07-dec-94
MITSUBISHI SB
112
C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-
1971
C 21-aug-85
MITSUBISHI SB
114
Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.
MITSUBISHI SB
119
The Bolt and Bolt Hole Diam. of Nose
L.G
JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model
MITSUBISHI SB
123
Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n
MITSUBISHI SB
124
Scissors Switch,Nose L.G. -Install. of 31-aug-70 21-aug-85 N/A
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2012-12-06
Document number Page
164(195)
MITSUBISHI SB
128
B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n
MITSUBISHI SB
143
B Top Coating, Wing Integral Main F.T.-
SIo
JCAB AD TCD-0730-1-72 JCAB AD TCD-
0730-2-86
05-jan-72 B 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB
162
A Flex. Shafts, Flap Control Sys.-Insp. of
(AD750201)
JCAB AD TCD-0947A-74 LFV LVA828 Rev
A
03-Oct-
1974
A 27-jan-86 N/A due to S/N
MITSUBISHI SB 163
B Insp. of Outer Pane, Front Winds. & Inst FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV
LVA829 Rev A
16-nov-78 21-aug-85 N/A
MITSUBISHI SB
165
A Lubr. Interval,Wheel Bearing,Main &
Nose
24-jul-80 21-aug-85 N/A
MITSUBISHI SB
167
D Flap M.Jack Screw-Insp. of and/or Main
G
FAA, U.S AD 75-16-13 JCAB AD TCD-
1094A-76 LFV LVA1011 Rev A
24-jul-80 D 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
MITSUBISHI SB
168
A Propeller Pitch Control Lever-Insp. of
(AD761620)
FAA, U.S AD 75-16-20 JCAB AD TCD-
1188-75 LFV LVA1012
24-jul-80 A 21-aug-85
MITSUBISHI SB
169
B Shimmy Damper-Insp. and Modification
of
JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW
MITSUBISHI SB 170
A MLG Forward Door Em.Op. Cable-Insp. & Re (AD762204)
JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 21-aug-85 N/A N/A due to s/n
MITSUBISHI SB 171
B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 LFV LVA1014 Rev A
17-nov-77 B 21-aug-85
MITSUBISHI SB 173
A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 21-aug-85
MITSUBISHI SB
174 PART 1
C Tip Tank Conduit Tube-Insp.of,and
Rew.of (AD830902)
FINNISH AD M 1177/83 JCAB AD TCD-
1370A-81 LFV LVA1196
02-Oct-
1981
C 27-jan-86 N/A by s/n
MITSUBISHI SB
174 PART 2
C Tip Tank Conduit Tube Rework 02-Oct-
1981
C 27-jan-86 N/A N/A by A/C S/N
MITSUBISHI SB
175
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
JCAB AD TCD-1353-76 26-jun-76 21-aug-85
MITSUBISHI SB
176
E Elevator Trim Tab Bracket-Repl. of
LVD1971, AD 84-25-02, SB 031/27-005R1
FAA, U.S AD 84-25-02 FINNISH AD M
1080/82 JCAB AD TCD-1001A-76 JCAB AD TCD-1001B-2-84 LFV LVD1971
26-sep-84 E 21-aug-85
MITSUBISHI SB 177
B Mod. of Engine Nacelle Tail Area (AD810601)
JCAB AD TCD-1379-1-80 LFV LVA1197 Rev A
11-sep-80 B 27-jan-86
MITSUBISHI SB 179
Rodd Assem., Engine Nacelle Upper D.-R&M
27-May-1977
21-aug-85
MITSUBISHI SB 180
A Link, Engine Nacelle Upper D.-Repl. of (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 JCAB AD TCD-1520A-77 LFV
LVA1014 Rev A
17-nov-77 A 21-aug-85
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2012-12-06
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MITSUBISHI SB
181 PART 2
B Insp. and Repl. of Nose L.G. Strut Assem
(AD801812)
FAA, U.S AD 86-15-03 JCAB AD TCD-
1768-1-85 LFV LVA1546
08-apr-85 B 27-May-1986
MITSUBISHI SB
182
Add. of Ceiling Cover, Rear Bagg. Comp. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 27-May-1986 N/A N/A due to s/n.
MITSUBISHI SB
184
Turnbuckle, Control Cables -Repl. of 04-apr-80 21-aug-85
MITSUBISHI SB 188
Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 27-aug-84
MITSUBISHI SB
189
C Flap Control Torque Tube AD 88-23-01,
SB 067/27-008
FINNISH AD M 2722/00 JCAB AD TCD-
2252-1-87 JCAB AD TCD-2252-83 LFV
LVA1873 LFV LVD2202
28-jun-94 C 11-mar-96
MITSUBISHI SB
191
Engine El. Wire-Insp. and Replacement
of (AD820802)
JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 27-aug-84
MITSUBISHI SB
193
B Landing Gear Warning Horn Syst.Modif. 15-jun-94 B 04-dec-00 Rev A är utförd.
MITSUBISHI SB
194
Master Cauting Light Visibility-Impr. of 23-aug-82 27-aug-84
MITSUBISHI SB 196
A Ret. of coupling nut on the bleed air tu AD 84-12-04, SB 047/30-001
FAA, U.S AD 84-12-04 JCAB AD TCD-2342-1-84 JCAB AD TCD-2342-84 LFV
LVA1942 MAI SB 047/30-001 Rev A
12-apr-84 A 27-jan-86
MITSUBISHI SB
198
Add. Seal & Torque Insp. of Flap Flex.Sh
LVD2037, AD 87-04-03, SB 051/27-007
FAA, U.S AD 87-04-03 JCAB AD TCD-
2451-85 LFV LVD2037
13-feb-85 27-aug-84
MITSUBISHI SB
199
A Engine Lubricating Tubing Insp. &
Protec
24-jun-94 A 06-nov-09 PCW
MITSUBISHI SB
200
B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 07-Oct-1988
MITSUBISHI SB
201
A Generator Circuit Wires Insp. and Mod. FAA, U.S AD 87-12-02 JCAB AD TCD-
2545-1-88 LFV LVD2191
02-mar-88 A 24-mar-09 N/A by s/n
MITSUBISHI SB 204
Speed Placard Change 03-mar-87 02-May-1988
MITSUBISHI SB 206
Bendix Autop.Disengagement Method Stand.
FAA, U.S AD 88-13-01 JCAB AD TCD-2856-1-97 LFV LVD2190
13-Oct-1987
06-nov-09 N/A Due to model
MITSUBISHI SB 207
Rudder T.T. & Elevator T.T. Insp. & Rep. 20-May-1988
11-feb-10
MITSUBISHI SB 209
B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model
MITSUBISHI SB 210
A Engine Ignition Unit Replacement 12-nov-96 06-mar-98
MITSUBISHI SB
211
Rudder Trim Tab Modification (LVD
2338)
JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A N/A by s/n.
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166(195)
MITSUBISHI SB
212
A Insp of Anti-ice/Deice Systems (LVD
2347),
JCAB AD TCD-3393A-96 LFV LVD2347
Rev 1
25-apr-96 A 26-May-2010
MITSUBISHI SB
214
Engine Control Rod Inspection 06-dec-91 01-sep-92
MITSUBISHI SB
215
Removel of Prop. Governor Speed
Signal
23-Oct-
1991
28-feb-92
MITSUBISHI SB 216
Elevator Trim Tab Installation (LVD 2450
FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV
LVD2450 LFV LVD2537 LFV LVD2898
11-sep-92 07-May-1993
MITSUBISHI SB
218
A Propeller Feathering Linkage Inspection 17-jan-94 A 25-apr-94
MITSUBISHI SB
219
A Emergency Gear Down G.box Lower Pin
Repl
JCAB AD TCD-3942-1-94 JCAB AD TCD-
3942-94 LFV LVD2538 LFV LVD2592
24-Oct-
1994
A 27-mar-95
MITSUBISHI SB
221
Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 25-apr-94
MITSUBISHI SB
223
Pitot/Static System Improvement SR
064
MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 27-mar-00
MITSUBISHI SB 224
C Acrylic Windsheild/Window glass Insp. FAA U.S AD 2003-17-04, FINNISH AD M 3076, JCAB AD TCD-4311-95, LFV
LVD2678
30-apr-98 C 08-mar-11
MITSUBISHI SB
225
Forward fitting bult of wingtip tank LVD
2688
FAA, U.S AD 98-20-39 FINNISH AD M
2351/96 JCAB AD TCD-4310-96 LFV LVD2688
29-sep-95 04-dec-96
MITSUBISHI SB 226
E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97
FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD-
2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A
18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n.
MITSUBISHI SB 227
Rudder Torque Tube Modification 20-dec-96 10-apr-97
MITSUBISHI SB 228
Elevator Trim Indicator Modification LFV 2898
FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898
13-jul-98 09-nov-98
MITSUBISHI SB 229
Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689
20-feb-96 30-jul-96
MITSUBISHI SB 230
Mod.of Bearing Box Ldg. Gear Act. LVD 2819
JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 18-mar-98
MITSUBISHI SB 231
B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M
2786/00 JCAB AD TCD-4625A-2001 LFV
11-dec-02 B 03-mar-03 SL 079 performed earlier.
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
167(195)
LVD3122
MITSUBISHI SB
232
A De-Ice System Modification LVD 2800,
TCD-4626-97
FAA, U.S AD 2000-09-15 Rev 1 FINNISH
AD M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004
06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev
0.
MITSUBISHI SB 233
B Insp.of Engine Torque Indication System. TCD-4889-98, LFV 2924
FAA, U.S AD 2006-17-01 FINNISH AD M 2608/98 JCAB AD TCD-4889-2-2007
JCAB AD TCD-4889-98 LFV LVD2924
08-mar-07 B 18-apr-07 Checked, previously carried out
MITSUBISHI SB 234
Fl.Check of the Flight Idle Fuel Flow Se TCD-4890-98, LVD 2925
FAA, U.S AD 2006-17-05 JCAB AD TCD-4890-98 LFV LVD2925
07-Oct-1998
11-feb-10
MITSUBISHI SB 235
Inspection of landing gear power train JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model
MITSUBISHI SB 236
Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 18-Oct-2001
MITSUBISHI SB 237
Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02
MITSUBISHI SB 238
Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.
MITSUBISHI SB 239
Pneumatic Line Insp. and Modification JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 02-Oct-2003
MITSUBISHI SB 240
Inst.of Trottle Quadrant Placard 26-feb-03 02-Oct-2003
MITSUBISHI SB 241
A Inspection of Wing Attachment Hardware
FAA, U.S AD 2006-13-15 JCAB AD TCD-7030-2006
21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie
MITSUBISHI SL
060
System 17-feb-89 20-aug-91
MITSUBISHI SL
078
Automatic Autopilot Disconnect System 28-jan-02 26-May-2010
MITSUBISHI SL
079
Diode inst.in Flap Position Ind.Curcuit 28-jan-02 15-May-2001 Carried out by Mitsubishi (manufacturing-
made)
MITSUBISHI SL
080
Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.
MITSUBISHI SL
084
Pneumatic De-Ice Monitoring System 14-jun-04 26-May-2010
MITSUBISHI SL
085
Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-
2005
20-sep-05
MITSUBISHI SN 053
B Rudder Torque Tube AD 86-20-01, SB 020/34-005
05-nov-86 B 22-dec-87
MITSUBISHI SN 117
D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD TCD-4753-98 LFV LVD2922
14-jun-04 D 17-May-2004
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
168(195)
MITSUBISHI SN
146
Water Ingress into Vertical Stabilizer 19-dec-03 24-feb-04
MITSUBISHI SN
148
Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB
MITSUBISHI SN
156A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MITSUBISHI SN 157
Torque Indicating System Shift Potential 20-nov-08 11-mar-09 SB 233 considered
MITSUBISHI SN
161
Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE
MITSUBISHI SR
053A
Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 LFV LVD2015 Rev B MAI SR
020/34-005 MITSUBISHI SB 223
23-Oct-
1984
08-May-1998
MITSUBISHI SR
064
Pitot & Static System MITSUBISHI SB 223 30-apr-85 27-mar-00
MITSUBISHI SR
065
Warning Horn 20-jan-86 22-dec-87
MITSUBISHI SR 067
Emergency Exit Placard 17-sep-85 27-May-1986
MITSUBISHI SR 072
Air Filter Replacement for Vacuum Syst. 25-apr-00 24-feb-04
MITSUBISHI SR 075
Inst. tip tank placard 29-Oct-2004
04-apr-05
MITSUBISHI STC
SA01913SE
Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-09 11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection
NARCO, Narco
NARCO SB ELT10-
16
ELT ASSY 18-apr-88 14-jun-91 N/A
NYGE, Saab Aerotech Aircraft
Services
NYGE TDM 00-09 Operatörsplats MU-2 11-apr-00 12-jan-00
NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 08-Oct-1999
NYGE TDM 02-24 Installation Moving MAP 10-Oct-
2002
29-Oct-2002
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
169(195)
NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04
NYGE TDM 03-08 8 GNS430/530 & MODE S
GTX330 install.
04-mar-03 20-Oct-2008
NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05
NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26)
20-nov-06 A 07-feb-08
NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07 A 07-feb-08
NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 07-mar-08
NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 07-sep-09
NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 20-Oct-2008 Original compliance with TDM rev A. Rev B does not affect previous complaiance.
NYGE TDM 09-02 C U-95 SORC Lite MU-2B 15-dec-09 C 29-apr-10 Original compliance I.A.W rev is not affected by rev C.
NYGE TDM 09-07 A GPS Splitter 18-May-2009
A 10-jun-09
NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 01-Oct-2010
NYGE TDM 10-03 A Pressure Bulkhead Feed Through
04-May-2010
A 04-Oct-2010
NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May-2010 C/W
NYGE TDM 11-35 A Terminating resistor A 27-Jan-12
NYGE TDM 12-21 A Avinstallation IK 14-Aug-12
NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 08-mar-11
NYGE TDM 97-01 TAPS 20-feb-97 01-jan-98
NYGE TDM 99-09 Installation BRNAV MU-2 01-nov-99 30-Oct-1999
NYGE TVO 1/09 Inspektion av Stringers &
struktur vinge
25-feb-09 02-mar-09 Inspected u/a
NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 07-May-1993
NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 20-apr-99
NYGE TVO 1/97 3 De-Icertank MU-2B,
korrosionskontroll
12-feb-97 11-feb-97
NYGE TVO 2/00 Märkning av infästning domkraft Mu2
01-dec-00 29-jan-01
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
170(195)
NYGE TVO 2/07 A Prevent FR31 radio to xmit
when RM2 off
06-feb-07 A 27-feb-07
NYGE TVO 2/10 1 Visual inspection of center
wing
19-apr-10 08-mar-11
NYGE TVO 2/91 A/C Elecrical System 10-jan-91 26-apr-91
NYGE TVO 3/06 Inspect lower rudder hinge
bracket
07-dec-06 08-mar-11
NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 11-feb-10
NYGE TVO 4/11 A Static inverter controll A 15-Dec-11
NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 07-dec-91
NYGE TVO 4/92 Engine Install. Kontr.
rörledningar
29-apr-92 19-May-1992
NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 11-feb-10
NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning.
25-Oct-1996
26-aug-97 Utförd tidigare (ref. Ove N lista)
NYGE TVO 6/88 Allm. instruktion för metallpropeller
13-jun-88 08-mar-11
NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-1992
19-Oct-1992
NYGE TVO 7/05 RMI-nål park. ej / ILS frekvens är vald
11-nov-05 25-nov-05 Carried out i.a.w. drawing NA-MF-199-008 & NA-MF-199-009
NYGE TVO 7/93 Starter Drive Splines 01-nov-93 07-dec-94
NYGE TVO 8/92 Wheel Parts 27-Oct-1992
07-May-1993
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
171(195)
2.7 GFE Aircraft Mitsubishi MU-2 SE-IUA
2.7.1 Aircraft Specification Type: Serial
Number:
Registration: Airframe
total Hours:
Total
Landing
Cycles:
Date
Reference:
MU-2B-26 345 SE-IUA 10619 4226 2012-11-23
2.7.2 Engines Type: Honeywell TPE331-6-252M
Serial
Number:
Total Hours
Since New:
Total
Cycles
Since New:
Hours remaining
overhaul/HSI/GBI:
Left Engine P20461 10937 9971 2876/667/2467
Right Engine P20502 7706 8168 439/835/2317
2.7.3 Propeller Type Number: Serial Number: Overhaul Due Date:
Left Propeller HC-B3TN-5E BVA 6325 2013-11-25
Right Propeller HC-B3TN-5E BVA 6194 2013-01-07
2.7.4 Avionics System: Type / Part Number: Note:
Autopilot & Flight Director Bendix M4D
COM/NAV/GPS 1 & 2 Garmin GNS 430
Audiopanel Bendix/King KMA-24H-70
MKR Bendix/King KMR 675
DME Bendix/King KN 63
ADF Bendix/King KR 87
XPDR 1 Garmin GTX 330D
XPDR 2 Garmin GTX 330 *)
RDR ALT Bendix/King KRA-10A
ELT Kanad ELT 406-AF-H
Airspeed Indicator LH / RH Aerosonic 20040-0113 / 20040-
0161
Altimeter LH Aerosonic 101735-01555
Altimeter incl. encoder RH United Instr. Inc. 5035P-P40
Altitude Reporter Ameri-King AK-350
Altitude Alerter Century 1D960
Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3
Attitude Gyro & Flight Director Ind. Bendix GH-14
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
172(195)
LH
Attitude Gyro Ind. RH AIM 504-0006-914
Turn & Bank Ind. LH Bendix 4099-B
Horizontal Situation Indicator LH Bendix RD-44
DG-Gyro Sperry C-14A
RMI Indicator Collins 332C-10
RMI/ADF adapter Bendix/King KDA-692
CDI Indicator Garmin GI-106A
*) XPDR 2 without diversity configuration
2.7.5 Mission System System: Description:
Fixed general installations
VHF/UHF COM FR31
GPS MAP
JET SI-3003B Inverter 115/200VAC 400Hz 3 phase
Laser Prism
MIL-STD-1553 Bus LH Wing Pylon
Wing Pylon
NATO 14” Alcon Ejector Unit LH and RH Wing Pylon
EW system
ADRIAN Pod mounted system LH and RH Wing
Pylon
A100 Pod mounted system LH Wing Pylon
Missile Threat Simulator
DARTS Pod mounted system LH Wing Pylon
Chaff Dispenser
BOX 3 Pod mounted system LH and RH Wing
Pylon
Target Towing
MBV7S Inboard winch
AS200 MDI (Miss Distance Indicator)
Precisions GPS Pos System
TAPS
Radar Calibration System
GPS Sphere
2.7.6 Mission Cable Harness to Hard Points Used for Mission
System:
LH NATO Hard point: RH NATO Hard point: Note:
Adrian C & S, A100, DARTS
and BOX 3 General Signal Harness AWG22 shielded x 44
General Signal Harness AWG22 shielded x 50
A100 MIL-STD-1553B Data
Bus
Triax Cable x 1
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
173(195)
A100 and DARTS AC Power
115/200VAC 400 Hz 3-
Phase 3 x 10 A
AWG 16 x 4
twisted
AWG 16 x 2
AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200
A
DC Power 28 VDC 200
A
AWG 2 x 2
Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable
2.7.7 Antenna Layout
Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type
2012-12-06
Document number Page
174(195)
2.7.8 Inspection due times and dates Status date November 23
rd 2012.
Description Maint. RefC/Out date C/Out Hrs Due Hrs Due date
Aircraft SE-IUA
Vingstudie MU-2 AMP 10000 11000
100 Hour Inspection AMP 2012-04-18 10577 10679 2013-04-18
200 Hour Inspection AMP 2012-04-18 10577 10777,9 2013-05-04
600 Hour Inspection AMP 2010-10-06 10402 11002,9 2013-10-05
1000 Hour Inspection AMP 2008-04-03 10000 11000
1200 Hour Inspection AMP 2008-03-28 9961 11161,9
1800 Hour Inspection AMP 2011-07-29 10479 12300
2000 Hour Inspection AMP 2008-04-03 10000 11960
1 Year Inspection AMP 2012-04-23 10577
2 Year Inspection AMP 2011-04-18 10425
10 Year Inspection AMP 2007-06-19 8700
Engine S/N P-20461 Remaining
Engine Assembly (Overhaul) AMP 13495,6 2876,3
Engine Hot Section Inspection AMP 11286,3 667
Engine Gearbox Inspection AMP 13086,3 2467
Engine S/N P-20502
Engine Assembly (Overhaul) AMP 11059,2 439,9
Engine Hot Section Inspection AMP 11455 835,7
Engine Gearbox Inspection AMP 12936,34 2317,04
Propeller L/H O/H AMP 2008-11-19 14361,5 2013-11-25
Propeller R/H O/H AMP 2008-04-03 13834,7 2013-01-07
Unclassified Date FMV Document ID Subject type
2012-12-06 ange ange
Document number Page
ange 175(195)
2.7.9 Implemented Changes Status date November 23
rd 2012.
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Complianc
e
Statu
s
Remarks
SB/AD etc
Reference
Rev Subject Document reference Eff. date Rev Compliance Stat
us
Remarks
EASA, European Aviation
Safety Agency
EASA AD 2006-0265
Incorrect transponder altitude 30-aug-06
14-mar-09
EASA AD 2009-0251-E
Portable Fire Extinguishers-Ident/Repl 25-nov-09
07-May-2010 N/A N/A by current P/N installed
EASA AD 2009-0262
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09
07-May-2010 N/A N/A by current P/N installed
EASA AD 2009-0278
Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09
07-May-2010 N/A N/A by current P/N installed
EASA AD 2010-0003
R1 Mode S Transponder -Check/Modification
11-jan-10 R1 10-mar-10 N/A due to model
EASA AD 2012-0037
Kidde Gravinier hand operated fire extinguisher
4-May-12
EASA SIB 2008-58R1
Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN SSB0845 Rev IR
17-dec-08
21-sep-10 N/A by SSB 0844 incorporated
EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model
FAA, U.S, Federal
Aviation
Administration
FAA, U.S AD 2000-
02-25
AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b.
FAA, U.S AD 2000-09-15
1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M 2786/00 MAI SB 086/74-002 Rev A MAI SB
07-jul-00 1 22-nov-01 Action not required due to s/n.
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 176(195)
093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A
FAA, U.S AD 2003-17-04
Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 087/56-001 Rev B MITSUBISHI SB 224 Rev
C
01-Oct-2003
07-Oct-2010
FAA, U.S AD 2005-
14-12
Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 14-sep-05
FAA, U.S AD 2005-
18-20
Prop de-icer "FASTprop" 14-Oct-
2005
12-Oct-2005 N/A Due to boots p/n
FAA, U.S AD 2006-
13-15
Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB
241 Rev A
11-aug-
06
11-nov-02 c/o in conjunction with vingstudie
FAA, U.S AD 2006-15-07
Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06
24-aug-06 se Mitsubishi SB 229
FAA, U.S AD 2006-17-01
Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 Rev B
22-sep-06
21-sep-06 PCW see MSB 233A
FAA, U.S AD 2006-17-05
Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06
11-Oct-2010
FAA, U.S AD 2007-17-09
Reduce max deflect elev nose-down trim
MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07
11-sep-07 Previously carried out i.a.w. mentioned SB's.
FAA, U.S AD 71-14-01
Fuel Tank Fungus Coating Peeling 01-May-1972
01-jan-96 N/A N/A by s/n
FAA, U.S AD 75-03-06
Cracks and Optical Distortion LFV LVA829 Rev A 13-nov-74
15-jul-86 N/A N/A due to s/n.
FAA, U.S AD 75-16-13
Main Wing Flap JCAB AD TCD-1094A-76 05-aug-75
05-feb-02 N/A Ej tillämplig p.g.a. s/n.
FAA, U.S AD 75-16-20
Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 MITSUBISHI SB 168 Rev A
12-aug-75
10-nov-82
FAA, U.S AD 78-03-05
Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
23-feb-78 10-apr-87
FAA, U.S AD 81-06-01
1 Engine Aft Nacelles 01-apr-81
1 08-jun-87 Previously complied with
FAA, U.S AD 81-25-04
1 Engine's Electrical wiring SB 036/71-003A, SB 043/71-005
21-jan-82 1 27-mar-09 N/A by model
FAA, U.S AD 82-08-02
Electrical Wiring Inspection 15-apr-82
02-aug-82
FAA, U.S AD 83-08-01
2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD T5114/05 HARTZELL SI 140A Rev 9
28-apr-82
2 20-May-2005 Ref. MU2B MM chap 13.4 when using bolts P/N B-3339 only
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 177(195)
FAA, U.S AD 83-09-02
Strobe Light Assemblies 17-May-1983
27-mar-09 N/A by s/n
FAA, U.S AD 84-12-
04
Torque of Air Tube Coupling Nuts SB
047/30-001, SB 196A
MAI SB 047/30-001 Rev A MITSUBISHI SB
196 Rev A
28-jun-84 16-jun-87
FAA, U.S AD 84-25-
02
Elevator TrimTab Bracket Insp/Repl.
SB 031/27-005 R1, SB 176E
MAI SB 031/27-005 Rev 1 MITSUBISHI SB
176 Rev E
18-dec-
84
16-jun-86
FAA, U.S AD 86-15-
03
NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2
Rev B
13-aug-
86
15-jul-04 Found SB 181 part 2 PCW.
FAA, U.S AD 86-20-
01
To assure anti-ice capability of pitot
SB 020/34-005, SB 053A
LFV LVD2015 Rev B MAI SR 020/34-005
MITSUBISHI SR 053A
06-Oct-
1986
15-feb-00
FAA, U.S AD 86-26-
02
To prevent engine flameout in an
iceing SB 74-0003, SR 040/74-001
GARRETT SB 74-0003 Rev , MITSUBISHI SB
226 Rev E
31-dec-
87
09-mar-09 see applicable engine for c/o
FAA, U.S AD 87-04-
03
Addit. Seal and Flap Flexible Shaft
Insp SB 051/27-007, SB 198
MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-
87
16-May-1986
FAA, U.S AD 87-12-
02
Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 27-mar-09 N/A by s/n
FAA, U.S AD 88-13-
01
Bendix Autopilot Disengagement SB
066/22-006
LFV LVD2190 MAI SB 066/22-006 Rev A
MITSUBISHI SB 206
11-jul-98 03-mar-88
FAA, U.S AD 88-21-
01
1 To minimize confusion in
autopilot/manua SB 066/22-006
LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-jan-12
FAA, U.S AD 88-23-
01
To prevent flap control failure SB
067/27-008, SB 189B
LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-
88
14-sep-95
FAA, U.S AD 93-07-11
ELECTRIC TRIM SYSTEM SB 079/27-010
LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n
FAA, U.S AD 94-04-16
Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94
08-apr-93
FAA, U.S AD 94-11-04
Change of Flight Idle Blade Angel SB 016/61-001
LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n
FAA, U.S AD 96-25-02
Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-4552-96 LFV LVD2749
27-dec-96
12-nov-97
FAA, U.S AD 97-04-13
Vent Check Valve Assy LFV LVD2769 16-apr-97
05-May-1997 N/A N/A due to model.
FAA, U.S AD 97-20-14 CNL
Icing related incidents/accidents 17-Oct-1997
02-dec-98
FAA, U.S AD 97-25-
02
To prevent loss of airplane
ctrl/overspe
FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17
FAA, U.S AD 98-20-
39
Forward fitting bolt of wingtip tank SB
MU-2 225, 089/57-002A
LFV LVD2688 MAI SB 089/57-002 Rev A ,
MITSUBISHI SB 225
19-Oct-
1998
24-Oct-1996
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 178(195)
FINNISH, Finnish
Civil Aviation
Adm.
FINNISH AD M 2609/98
Justering av br,nslefl"de MHI SB 097/73-001, TCD-4890-98
JCAB AD TCD-4890-98 , MAI SB 097/73-001
12-nov-99
11-Oct-2010
FINNISH AD M 3076
Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 , MAI SB 087/56-001 Rev B , MITSUBISHI SB 224 Rev C
21-aug-03
07-Oct-2010
GARMIN, Garmin
GARMIN SB 0004 Incorp.of Main Software Version 2.16 01-May-
2000
18-May-2000
GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008-58R1 14-nov-
08
A 19-May-2010
GARRETT,
AlliedSignal
Aerospace
GARRETT SB 74-
0003
6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-
94
09-mar-09 see applicable engine for c/o
HARTZELL,
Hartzell Propeller
Inc.
HARTZELL SB 61-256
Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI SL 080
08-feb-02 13-maj-02 L/H side
HARTZELL SB 61-279 ALERT
4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL 085
04-Oct-2005
14-nov-05 propellerbolts previously checked u/a
HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 Rev A
30-mar-05
9 13-mar-08 see previously revision
JCAB, Japan Civil
Aviation Bureau
JCAB AD TCD-0518-68
Rivet holes elevator hinge fitting 06-feb-68 26-mar-09 N/A by s/n
JCAB AD TCD-0642-70
AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 16-jul-86 N/A by s/n
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 179(195)
JCAB AD TCD-0643-70
Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A N/A by s/n.
JCAB AD TCD-
0652-70
Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-
70
26-mar-09 N/A by model
JCAB AD TCD-
0653-70
Engine Nacelle Tail Area-Modification
of
25-mar-
70
26-mar-09 N/A by model
JCAB AD TCD-
0660-70
Replacement of bearing in
nosegearstrut
LFV LVA457 MITSUBISHI SB 123 01-May-
1970
26-mar-09 N/A by s/n
JCAB AD TCD-
0730-1-72
Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev
B
25-mar-
72
14-jul-04 N/A N/A by s/n.
JCAB AD TCD-
0730-2-86
Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-
86
26-mar-09 N/A by s/n
JCAB AD TCD-
0859-72
Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-
72
10-sep-72 N/A N/A due to model.
JCAB AD TCD-
0866-72
NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-
1972
31-dec-72 N/A N/A due to model.
JCAB AD TCD-
0947A-74
Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev
A
12-nov-
74
06-Oct-1987 N/A N/A due to s/n.
JCAB AD TCD-
0948A-1-78
Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-
78
26-mar-09 N/A by s/n
JCAB AD TCD-
0948A-74
Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev
B
07-Oct-
1974
15-jul-86 N/A N/A due to s/n.
JCAB AD TCD-1001A-76
Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev E
06-Oct-1976
16-jun-86
JCAB AD TCD-1001B-2-84
Replacement of Elevator Trim Tab Bracket
FINNISH AD M 1080/82 LFV LVD1971 MITSUBISHI SB 176 Rev E
12-dec-84
16-jun-86
JCAB AD TCD-1094A-76
Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A MITSUBISHI SB 167 Rev D
06-sep-76
05-feb-02 N/A Ej tillämplig p.g.a. s/n.
JCAB AD TCD-1188-75
Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 MITSUBISHI SB 168 Rev A
06-May-1975
10-nov-82
JCAB AD TCD-1202-75
Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB
180 Rev A
20-sep-75
15-jul-04 Found SB 171 and SB 180 PCW.
JCAB AD TCD-
1209-75
Insp/mod of NLG shimmydamper
locking
LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 08-jun-87
JCAB AD TCD-
1235-75
Insp./repl. of MLG fwd door
emerg.cables
LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-
75
10-apr-78 N/A N/A due to model.
JCAB AD TCD-1272-75
Supp.,MLG Forward D. Actuating Mech.-I&M
MITSUBISHI SB 172 14-nov-75
26-mar-09 N/A by model
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 180(195)
JCAB AD TCD-1284-1-76
Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76
28-Oct-2009 N/A Due to S/N
JCAB AD TCD-
1328-76
Fire hazard in rear baggage
compartment
01-jul-76 26-mar-09 N/A by s/n
JCAB AD TCD-
1353-76
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
MITSUBISHI SB 175 16-aug-
76
26-mar-09
JCAB AD TCD-
1370-76
Inspect strobelight conduit in Tiptank LFV LVA1196 18-Oct-
1976
06-Oct-1987 N/A by s/n
JCAB AD TCD-
1370A-81
Inspect strobelight conduit in Tiptank
supersed TCD-1370-76
MITSUBISHI SB 174 PART 1 Rev C 05-nov-
81
24-mar-09 N/A by s/n
JCAB AD TCD-
1379-1-80
Insp. rear eng. cowling reg.
heatdamage
LFV LVA1197 Rev A MITSUBISHI SB 177
Rev B
06-feb-02 08-jun-87
JCAB AD TCD-
1520A-77
Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-
77
24-mar-09 ref. SB 180
JCAB AD TCD-
1768-1-85
Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.
JCAB AD TCD-
1817-79
Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 08-jun-87 N/A N/A due to s/n.
JCAB AD TCD-
2048-81
Insp. firewarning & emerg.power
circuit
LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-1981 N/A N/A due to s/n.
JCAB AD TCD-
2070-81
Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 16-May-1986
JCAB AD TCD-2113-82
Insp./replace engine electrical harness
LFV LVA1788 MITSUBISHI SB 191 06-feb-02 16-May-1986
JCAB AD TCD-2252-2-88
Flap system torquetubes supersed TCD-2252-1-87
01-feb-89 24-mar-09 PCW
JCAB AD TCD-2252-83
Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 14-sep-95
JCAB AD TCD-2263-83
NLG. bracket attaching to drag strut 13-aug-83
24-mar-09 N/A by model
JCAB AD TCD-2342-1-84
Engine inlet anti-ice tubing. Torq./lock
MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW
JCAB AD TCD-2342-84
Engine inlet anti-ice tubing. Torq./lock
LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 16-jun-87
JCAB AD TCD-
2450A-87
Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.
JCAB AD TCD-
2451-1-87
Add. seal/Tq. insp of flap flex. shaft 01-May-
1987
09-mar-09 PCW see TCD-2451-85
JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30-sep- 16-May-1986
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 181(195)
2451-85 Superseeded by TCD-2451-1-87 85
JCAB AD TCD-2545-1-88
Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 24-mar-09 N/A by s/n
JCAB AD TCD-2679A-97
Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 MITSUBISHI SB 226 Rev E
01-feb-97 22-nov-01
JCAB AD TCD-2856-1-97
Bendix M4C Autopilot System MITSUBISHI SB 206 05-nov-97
28-Oct-2009 N/A Due to model
JCAB AD TCD-3378-90
Insp./mod. of rudder trimtab leadingedge
LFV LVD2338 MITSUBISHI SB 211 28-mar-91
14-jul-04 N/A N/A by s/n.
JCAB AD TCD-3393A-96
Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 1 MITSUBISHI SB 212 Rev A
25-May-1996
07-Oct-2010
JCAB AD TCD-3464-91
Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model
JCAB AD TCD-
3740A-98
Mod.of Autopilote pitchtrimsystem
MSB 216, 228 LVD 2898
FINNISH AD M 2581/98 LFV LVD2450 LFV
LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228
17-aug-
98
18-nov-98
JCAB AD TCD-3901-93
Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 MITSUBISHI SB 221
10-sep-93
01-feb-94
JCAB AD TCD-3942-1-94
Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 MITSUBISHI SB 219 Rev A
28-nov-94
01-feb-94
JCAB AD TCD-3942-94
Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 01-feb-94
JCAB AD TCD-4310-96
Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 MITSUBISHI SB 225
01-apr-96
24-Oct-1996
JCAB AD TCD-
4311-95
Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678
MITSUBISHI SB 224 Rev C
01-nov-
95
07-Oct-2010
JCAB AD TCD-
4379-96
Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01-apr-
96
30-jul-96
JCAB AD TCD-
4552-96
Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-
96
12-nov-97
JCAB AD TCD-
4625-97
Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB
093/22-009
14-jul-97 09-feb-01
JCAB AD TCD-
4625A-2001
Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B
NYGE TDM01-45
16-mar-
01
13-mar-09 PCW
JCAB AD TCD-4626-97
De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800 MITSUBISHI SB 232 Rev A
01-May-1997
14-jul-04 PCW
JCAB AD TCD-4684-97
Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 MITSUBISHI SB 230
01-jun-97 25-mar-99
Öppen/Unclassified Datum Diarienummer Ärendetyp
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Dokumentnummer Sida
ange 182(195)
JCAB AD TCD-4753-98
Ändring av flyghandbok LVD 2922,FAA AD 97-20-14, MHI SN 117A
FINNISH AD M 2518/98 LFV LVD2922 MITSUBISHI SN 117 Rev D
18-feb-98 02-dec-98 FAA AD utförd.
JCAB AD TCD-
4753A-2004
Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 11-dec-03
JCAB AD TCD-
4838-98
Inspection of landing gear power
train
FINNISH AD M 2574/98 LFV LVD2897
MITSUBISHI SB 235
04-aug-
98
24-mar-09 N/A by model
JCAB AD TCD-
4889-2-2007
Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.
JCAB AD TCD-
4889-98
Insp. of Engine Torque Indication
System LFV 2924, MU SB 233
FINNISH AD M 2608/98 LFV LVD2924
MITSUBISHI SB 233 Rev B
05-nov-
98
14-jul-04 PCW
JCAB AD TCD-
4890-98
Check of flight idle FF LVD 2925, MU
SB 234
FINNISH AD M 2609/98 LFV LVD2925 04-nov-
98
11-Oct-2010
JCAB AD TCD-
5030-99
Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-
1999
24-mar-09 N/A by model
JCAB AD TCD-
5432-2000
AFM revision LFV LVD3112 27-nov-
00
12-feb-02
JCAB AD TCD-
5547-2001
To prevent loss of airplane control LFV LVD3123 16-mar-
01
12-feb-02
JCAB AD TCD-
5747-2001
Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-
01
10-Oct-2001
JCAB AD TCD-
5864-2001
Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-
01
17-jan-02
JCAB AD TCD-6127-2003
Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03
09-sep-03
JCAB AD TCD-7030-2006
Inspection of Wing Attachment Hardware
MITSUBISHI SB 241 Rev A 27-dec-06
17-jan-07 c/o in conjunction with wingstudie
LFV,
Luftfartsverket
LFV LVA 1011 A Kontroll av vingklaffarnas manöversystem
FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 MITSUBISHI SB 167 Rev D
05-feb-02 A 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
LFV LVA 1012 Kontroll av propellerreglagets montering
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 MITSUBISHI SB 168 Rev A
05-feb-02 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 Rev B
05-feb-02 08-jun-87
LFV LVA 1014 A Kontr. & byte av motorinkl.
låsanordning
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A
05-feb-02 A 10-apr-87
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Dokumentnummer Sida
ange 183(195)
LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A
05-feb-02 10-apr-78 N/A N/A due to s/n
LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174
PART 1 Rev C
06-feb-02 06-Oct-1987 N/A by s/n
LFV LVA 1197 A Förhindr. av värmeskador på
bak.motorpl.
JCAB AD TCD-1379-1-80 MITSUBISHI SB
177 Rev B
06-feb-02 A 08-jun-87
LFV LVA 1238 Kontr. & byte av infästningsdet.
trimrod
06-feb-02 21-apr-09 N/A by s/n
LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-
1-85 MITSUBISHI SB 181 PART 2 Rev B
06-feb-02 08-jun-87
LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 08-jun-87 N/A N/A due to s/n.
LFV LVA 1740 Kontr.av brandvarnings-och n"dstr"mskret
JCAB AD TCD-2048-81 MITSUBISHI SB 187 Rev B
05-feb-02 31-aug-09 N/A by s/n
LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 16-May-1986
LFV LVA 1788 Kontroll/Utbyte av elledningar på motor
JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 02-aug-82
LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB 189 Rev C
06-feb-02 14-sep-95
LFV LVA 1942 Momentdragning/låsn.av koppl.i
varmlufts
JCAB AD TCD-2342-84 MITSUBISHI SB 196
Rev A
06-feb-02 16-jun-87
LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 16-jul-86 N/A N/A by s/n
LFV LVA 439 Rev. av flyghandbok betr. bränslespec.
JCAB AD TCD-0642-70 MITSUBISHI SB 112 Rev C
05-feb-02 16-jul-86 N/A by model
LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model
LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n
LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.
LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 08-dec-09 N/A by A/C serial number
LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n & model
LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB
162 Rev A
05-feb-02 A 06-Oct-1987 N/A N/A due to s/n.
LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-
06 JCAB AD TCD-0948A-74 MITSUBISHI SB
163 Rev B
05-feb-02 A 15-jul-86 N/A N/A due to s/n.
LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 16-jun-86
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ange 184(195)
LFV LVD 1238 Kontr./byte infästn.det. höjdtrimroder
15-apr-77
27-mar-09 N/A se LVA 886A & FAA AD 84-25-02
LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 18-jan-85 16-jun-86
LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005 Rev A, MHI SR 53
FAA, U.S AD 86-20-01 JCAB AD TCD-2450A-87 MAI SR 020/34-005 MITSUBISHI
SR 053A
24-May-1985
B 29-jan-87
LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85
16-May-1986
LFV LVD 2069 Altimeter 25-mar-86
18-aug-87 N/A N/A by p/n & s/n
LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA
26-jan-87 06-Oct-1987
LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006 och SB 206
FAA, U.S AD 88-13-01 MAI SB 066/22-006 Rev A MITSUBISHI SB 206
19-aug-88
03-mar-88
LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB 201 Rev A
19-aug-88
24-mar-09 N/A by s/n
LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-1-87 MAI SB 067/27-008 Rev A
MITSUBISHI SB 189 Rev C
08-dec-88
14-sep-95
LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-Dec-1988
12-feb-02
LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB
211
JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91
14-jul-04 N/A N/A by s/n.
LFV LVD 2347 1 Control Deice-system Mitsubishi SB
212A
JCAB AD TCD-3393A-96 MITSUBISHI SB
212 Rev A
29-May-
1996
1 07-Oct-2010
LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13
CHPT 9
23-May-
1991
19-jun-91 checked OK.
LFV LVD 2450 Elevator Trim Tab Installation MU SB
216
JCAB AD TCD-3740A-98 MITSUBISHI SB
216
03-dec-
92
08-apr-93
LFV LVD 2477 Electric Trim System AD930711, MU SB 079/27-0-010
FAA, U.S AD 93-07-11 MAI SB 079/27-010 03-jun-93 27-mar-09 N/A by s/n
LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93
16-nov-94
LFV LVD 2537 Reducering av Höjdrodrets trimområde. FAA AD 94-04-16, SB
216
FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94
08-apr-93
LFV LVD 2538 Byte Låspinne i landställets nödutf. SB
219
JCAB AD TCD-3942-94 MITSUBISHI SB 219
Rev A
07-apr-
94
01-feb-94
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Dokumentnummer Sida
ange 185(195)
LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n
LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox TCD-3942-1-94, MSB 219A
JCAB AD TCD-3942-1-94 MITSUBISHI SB 219 Rev A
09-feb-95 01-feb-94
LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB 224 Rev A
FAA, U.S AD 2003-17-04 JCAB AD TCD-4311-95 MITSUBISHI SB 224 Rev C
12-mar-96
07-Oct-2010
LFV LVD 2688 Kontr/byte av infästn.bult för tiptank MU-2 SB 225
FAA, U.S AD 98-20-39 JCAB AD TCD-4310-96 MITSUBISHI SB 225
09-May-1996
24-Oct-1996
LFV LVD 2689 Kontroll av linkage för prop.flöjning MU-2 SB 229
JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-1996
30-jul-96
LFV LVD 2732 Inspection/ Replacement of Prop Hub. FAA AD 96-18-14, Hz SB 136H
FAA, U.S AD 96-18-14 HARTZELL SB 61-261 Rev 1
27-sep-96
01-sep-99 Prop. utbytt mot BVA
LFV LVD 2749 Revision av flyghandbok AFM TCD-4552-96
FAA, U.S AD 96-25-02 JCAB AD TCD-4552-96
21-jan-97 12-nov-97
LFV LVD 2757 Sprickkontr. av landst,l.Side Brace
Stud AD 97-01-01
FAA, U.S AD 97-01-01 Rev 1 14-feb-97 12-nov-97
LFV LVD 2761 Installation av autoignition system
TCD-2679A-97
JCAB AD TCD-2679A-97 MITSUBISHI SB
226 Rev E
14-feb-97 29-mar-99
LFV LVD 2769 Demont.av backventil i
bränslesystemets MU-2 SB 130A
FAA, U.S AD 97-04-13 MITSUBISHI SB 130
Rev A
18-mar-
97
05-May-1997 N/A N/A due to s/n.
LFV LVD 2799 **RECOVERED RECORD** 09-feb-01
LFV LVD 2800 Mod. av De-ice Monitoring System
Mitsubishi SB 232, TCD-4626-97
JCAB AD TCD-4626-97 MITSUBISHI SB 232
Rev A
28-aug-
97
12-May-1998
LFV LVD 2819 Mod.av lagerboxar för
landställssystem Mitsubishi SB 230
JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-
97
12-jun-98
LFV LVD 2853 Periodisk funktionskontroll av
nödutgång
23-mar-
98
07-Oct-2010
LFV LVD 2897 Kontroll av landst,llets drivsystem
TCD-4838-98, SB 235
JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-
98
24-mar-09 N/A by model
LFV LVD 2898 Mod. av autopilotens höjdtrimsystem TCD-3740A-98, SB 216, 228
JCAB AD TCD-3740A-98 MITSUBISHI SB 216 MITSUBISHI SB 228
27-aug-98
18-nov-98
LFV LVD 2922 Änd.av Flyghandbok-Extra krav på typutbi TCD-4753-98, MHI SN 117A
JCAB AD TCD-4753-98 MITSUBISHI SN 117 Rev D
12-nov-98
02-dec-98 FAA AD utförd.
LFV LVD 2924 Kontr/Just av motorernas Torque indikeri MHI SB 233, TCD-4889-98
JCAB AD TCD-4889-98 MITSUBISHI SB 233 Rev B
01-dec-98
23-feb-00
LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id MHI SB 234
JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98
11-Oct-2010
LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209 Rev B
18-jun-99 24-mar-09 N/A by model
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 186(195)
LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02
LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-009 MITSUBISHI SB 231 Rev B NYGE
TDM01-45
02-apr-01
09-feb-01
LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-
01
12-feb-02
LFV LVD 3166 Sprickkontroll av infästning till ving-spetstank
JCAB AD TCD-5747-2001 MITSUBISHI SB 236
20-sep-01
10-Oct-2001
LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-012 MITSUBISHI SB 237
09-jan-02 17-jan-02
LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB 239
21-mar-03
09-sep-03
MAI, Mitsubishi
Aircraft
International
MAI SB 047/30-
001
A Torque of Bleed Air Tube Coupling
Nuts AD 84-12-04,SB 196A
FAA, U.S AD 84-12-04 MITSUBISHI SB 196
Rev A
19-jul-84 A 16-jun-87
MAI SB 051/27-
007
Add.Seal and Flap Flexible Shaft
Torque AD 87-04-03, SB 198
FAA, U.S AD 87-04-03 01-feb-85 16-May-1986
MAI SB 066/22-
006
A Bendix Autopilot Disengagement AD
88-13-01, AD 88-21-01 R1
FAA, U.S AD 88-13-01 FAA, U.S AD 88-21-
01 Rev 1 LFV LVD2190 MAI SB 069/24-006
06-jun-89 03-mar-89 Data transferred/updated on WO C05770
MAI SB 067/27-
008
A Insp/Repl. of Flap Control System
Torque AD 88-23-01, SB 189B
FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-
95
A 14-sep-95
MAI SB 069/24-006
Split Radio Bus Inspection and Rework
MAI SB 066/22-006 Rev A 17-nov-88
03-mar-88 N/A N/A due to Aircraft s/n
MAI SB 086/74-002
A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2435/97 MITSUBISHI SB 226 Rev E
05-Oct-2000
A 22-nov-01 Action not required due to s/n.
MAI SB 089/57-002
A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96
A 24-Oct-1996 N/A N/A due to s/n.
MAI SB 093/22-009
Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD JCAB AD TCD-4625-
97 LFV LVD3122 MITSUBISHI SB 231 Rev B
08-jul-97 09-feb-01
MAI SN 110/00-
017A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MAI SN 111/77-004
Torque Indicating System Shift Potential
20-nov-08
11-mar-09 SB 233 considered
MAI SR 020/34- Anti Ice Capability AD 86-20-01, SR FAA, U.S AD 86-20-01 LFV LVD2015 Rev B 06-Oct- 15-feb-00 N/A N/A due to s/n.
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 187(195)
005 053A MITSUBISHI SR 053A 1986
MITSUBISHI,
Mitsubishi Heavy
Industries Ltd
MITSUBISHI MSB
24-002
A **RECOVERED RECORD** A 18-jul-86 N/A
MITSUBISHI MSB
24-004
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB
27-001
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB
27-003
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB 27-005
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB 27-006
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB 27-007
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB 30-001
A **RECOVERED RECORD** A 18-jul-86 N/A
MITSUBISHI MSB 32-001
A **RECOVERED RECORD** A 18-jul-86 N/A
MITSUBISHI MSB 32-004
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB 32-006
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB 32-010
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB
34-004
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB
34-007
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB
54-001
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSB
54-002
A **RECOVERED RECORD** A 18-jul-86 N/A
MITSUBISHI MSB B **RECOVERED RECORD** B 18-jul-86 N/A
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 188(195)
71-003
MITSUBISHI MSB 71-005
**RECOVERED RECORD** 18-jul-86 N/A
MITSUBISHI MSR 066
B **RECOVERED RECORD** B 06-Oct-1987
MITSUBISHI SB 066
Bendix M4D 18-dec-87
06-mar-89 Info transfererad till SB 066/222-006 ref C05770
MITSUBISHI SB 076/22-008
M-4() Autop.Engage Switch Guard Install.
11-apr-91
16-nov-94
MITSUBISHI SB 112
C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-1971
C 16-jul-86
MITSUBISHI SB 114
Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.
MITSUBISHI SB
119
The Bolt and Bolt Hole Diam. of Nose
L.G
JCAB AD TCD-0652-70 LFV LVA456 10-mar-
70
26-mar-09 N/A by model
MITSUBISHI SB
123
Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-
70
26-mar-09 N/A by s/n
MITSUBISHI SB
124
Scissors Switch,Nose L.G. -Install. of 31-aug-
70
17-jul-86 N/A
MITSUBISHI SB
128
B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n
MITSUBISHI SB
143
B Top Coating, Wing Integral Main F.T.-
SIo
JCAB AD TCD-0730-1-72 JCAB AD TCD-
0730-2-86
05-jan-72 B 14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 162
A Flex. Shafts, Flap Control Sys.-Insp. of (AD750201)
JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-1974
A 06-Oct-1987 N/A
MITSUBISHI SB 163
B Insp. of Outer Pane, Front Winds. & Inst
FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV
LVA829 Rev A
16-nov-78
15-jul-86 N/A
MITSUBISHI SB
165
A Lubr. Interval,Wheel Bearing,Main &
Nose
24-jul-80 03-mar-77 N/A
MITSUBISHI SB
167
D Flap M.Jack Screw-Insp. of and/or
Main G
FAA, U.S AD 75-16-13 JCAB AD TCD-
1094A-76 LFV LVA1011 Rev A
24-jul-80 D 05-feb-02 N/A Ej tillämplig p.g.a. s/n.
MITSUBISHI SB
168
A Propeller Pitch Control Lever-Insp. of
(AD761620)
FAA, U.S AD 75-16-20 JCAB AD TCD-1188-
75 LFV LVA1012
24-jul-80 A 10-nov-82
MITSUBISHI SB 169
B Shimmy Damper-Insp. and Modification of
JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW
MITSUBISHI SB 170
A MLG Forward Door Em.Op. Cable-Insp. & Re (AD762204)
JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77
A 17-jul-86 N/A N/A due to s/n
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 189(195)
MITSUBISHI SB 171
B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 LFV LVA1014 Rev A
17-nov-77
B 10-apr-78
MITSUBISHI SB
173
A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 A 06-feb-06 N/A N/A due to s/n
MITSUBISHI SB
174 PART 1
C Tip Tank Conduit Tube-Insp.of,and
Rew.of (AD830902)
FINNISH AD M 1177/83 JCAB AD TCD-
1370A-81 LFV LVA1196
02-Oct-
1981
C 06-Oct-1987 N/A by s/n
MITSUBISHI SB
174 PART 2
C Tip Tank Conduit Tube Rework 02-Oct-
1981
C 06-Oct-1987 N/A N/A by A/C S/N
MITSUBISHI SB
175
Barrel Nut, Inner/Outer Wing Conn.-
Repl.
JCAB AD TCD-1353-76 26-jun-76 24-aug-76
MITSUBISHI SB
176
E Elevator Trim Tab Bracket-Repl. of
LVD1971, AD 84-25-02, SB 031/27-005R1
FAA, U.S AD 84-25-02 FINNISH AD M
1080/82 JCAB AD TCD-1001A-76 JCAB AD TCD-1001B-2-84 LFV LVD1971
26-sep-
84
E 16-jun-86
MITSUBISHI SB 177
B Mod. of Engine Nacelle Tail Area (AD810601)
JCAB AD TCD-1379-1-80 LFV LVA1197 Rev A
11-sep-80
B 08-jun-87
MITSUBISHI SB 179
Rodd Assem., Engine Nacelle Upper D.-R&M
27-May-1977
08-jun-78
MITSUBISHI SB
180
A Link, Engine Nacelle Upper D.-Repl. of
(AD780305)
FAA, U.S AD 78-03-05 JCAB AD TCD-1202-
75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A
17-nov-
77
A 10-apr-78
MITSUBISHI SB 181 PART 2
B Insp. and Repl. of Nose L.G. Strut Assem (AD801812)
FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 LFV LVA1546
08-apr-85
B 18-aug-87
MITSUBISHI SB 182
Add. of Ceiling Cover, Rear Bagg. Comp.
JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79
08-jun-87 N/A N/A due to s/n.
MITSUBISHI SB 184
Turnbuckle, Control Cables -Repl. of 04-apr-80
14-nov-86
MITSUBISHI SB 188
Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 16-May-1986
MITSUBISHI SB 189
C Flap Control Torque Tube AD 88-23-01, SB 067/27-008
FINNISH AD M 2722/00 JCAB AD TCD-2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202
28-jun-94 C 14-sep-95
MITSUBISHI SB 191
Engine El. Wire-Insp. and Replacement of (AD820802)
JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81
02-aug-82
MITSUBISHI SB 193
B Landing Gear Warning Horn Syst.Modif.
15-jun-94 B 04-dec-00 Rev A är utförd.
MITSUBISHI SB 194
Master Cauting Light Visibility-Impr. of
23-aug-82
16-May-1986
MITSUBISHI SB 196
A Ret. of coupling nut on the bleed air tu AD 84-12-04, SB 047/30-001
FAA, U.S AD 84-12-04 JCAB AD TCD-2342-1-84 JCAB AD TCD-2342-84 LFV LVA1942
12-apr-84
A 16-jun-87
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 190(195)
MAI SB 047/30-001 Rev A
MITSUBISHI SB 198
Add. Seal & Torque Insp. of Flap Flex.Sh LVD2037, AD 87-04-03, SB
051/27-007
FAA, U.S AD 87-04-03 JCAB AD TCD-2451-85 LFV LVD2037
13-feb-85 16-May-1986
MITSUBISHI SB
199
A Engine Lubricating Tubing Insp. &
Protec
24-jun-94 A 06-nov-09 PCW
MITSUBISHI SB 200
B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 19-Mar-12
MITSUBISHI SB 201
A Generator Circuit Wires Insp. and Mod.
FAA, U.S AD 87-12-02 JCAB AD TCD-2545-1-88 LFV LVD2191
02-mar-88
A 24-mar-09 N/A by s/n
MITSUBISHI SB 204
Speed Placard Change 03-mar-87
14-apr-89
MITSUBISHI SB 206
Bendix Autop.Disengagement Method Stand
FAA, U.S AD 88-13-01 , JCAB AD TCD-2856-1-97, LFV LVD2190
13-Oct-1987
28-Oct-2009 N/A Due to model
MITSUBISHI SB 207
Rudder T.T. & Elevator T.T. Insp. & Rep.
20-May-1988
07-Oct-2010
MITSUBISHI SB 209
B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99
B 24-mar-09 N/A by model
MITSUBISHI SB 210
A Engine Ignition Unit Replacement 12-nov-96
06-mar-98
MITSUBISHI SB 211
Rudder Trim Tab Modification (LVD 2338)
JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90
14-jul-04 N/A N/A by s/n.
MITSUBISHI SB 212
A Insp of Anti-ice/Deice Systems (LVD 2347),
JCAB AD TCD-3393A-96 LFV LVD2347 Rev 1
25-apr-96
A 07-Oct-2010
MITSUBISHI SB
214
Engine Control Rod Inspection 06-dec-
91
08-May-1992
MITSUBISHI SB
215
Removel of Prop. Governor Speed
Signal
23-Oct-
1991
08-May-1992
MITSUBISHI SB
216
Elevator Trim Tab Installation (LVD
2450
FAA, U.S AD 2007-17-09 FAA, U.S AD 94-
04-16 JCAB AD TCD-3740A-98 LFV LVD2450 LFV LVD2537 LFV LVD2898
11-sep-
92
08-apr-93
MITSUBISHI SB 218
A Propeller Feathering Linkage Inspection
17-jan-94 A 01-feb-94
MITSUBISHI SB 219
A Emergency Gear Down G.box Lower Pin Repl
JCAB AD TCD-3942-1-94 JCAB AD TCD-3942-94 LFV LVD2538 LFV LVD2592
24-Oct-1994
A 01-feb-94
MITSUBISHI SB
221
Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-
93
01-feb-94
MITSUBISHI SB
223
Pitot/Static System Improvement SR
064
MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 15-feb-00
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 191(195)
MITSUBISHI SB 224
C Acrylic Windsheild/Window glass Insp. UHB
FAA, U.S AD 2003-17-04 FINNISH AD M 3076 JCAB AD TCD-4311-95 LFV LVD2678
30-apr-98
C 07-Oct-2010
MITSUBISHI SB
225
Forward fitting bult of wingtip tank
LVD 2688
FAA, U.S AD 98-20-39 FINNISH AD M
2351/96 JCAB AD TCD-4310-96 LFV LVD2688
29-sep-
95
24-Oct-1996
MITSUBISHI SB 226
E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97
FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97
FINNISH AD M 2786/00 JCAB AD TCD-2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A
18-sep-01
E 22-nov-01 PCW no further action (rev.E) required due to s/n.
MITSUBISHI SB 227
Rudder Torque Tube Modification 20-dec-96
08-sep-97
MITSUBISHI SB 228
Elevator Trim Indicator Modification LFV 2898
FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV
LVD2898
13-jul-98 18-nov-98
MITSUBISHI SB
229
Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-
4379-96 LFV LVD2689
20-feb-96 30-jul-96
MITSUBISHI SB
230
Mod.of Bearing Box Ldg. Gear Act.
LVD 2819
JCAB AD TCD-4684-97 LFV LVD2819 05-mar-
97
12-jun-98
MITSUBISHI SB 231
B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M
2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE
TDM01-45
11-dec-02
B 03-mar-03 SL 079 performed earlier.
MITSUBISHI SB
232
A De-Ice System Modification LVD
2800, TCD-4626-97
FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD
M 2786/00 JCAB AD TCD-4626-97 LFV
LVD2800 MAI SB 096/30-004
06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev 0.
MITSUBISHI SB
233
B Insp.of Engine Torque Indication
System. TCD-4889-98, LFV 2924
FAA, U.S AD 2006-17-01 FINNISH AD M
2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924
08-mar-
07
B 18-apr-07 Checked, previously carried out
MITSUBISHI SB 234
Fl.Check of the Flight Idle Fuel Flow Se TCD-4890-98, LVD 2925
FAA, U.S AD 2006-17-05 JCAB AD TCD-4890-98 LFV LVD2925
07-Oct-1998
11-Oct-2010
MITSUBISHI SB 235
Inspection of landing gear power train
JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98
24-mar-09 N/A by model
MITSUBISHI SB
236
Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-
01
10-Oct-2001
MITSUBISHI SB
237
Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-
01
17-jan-02
MITSUBISHI SB
238
Main Landing Gear Door Safety Pin 05-dec-
02
09-jan-03 Perf. at each 600 h. insp.
Öppen/Unclassified Datum Diarienummer Ärendetyp
2012-12-06 ange ange
Dokumentnummer Sida
ange 192(195)
MITSUBISHI SB 239
Pneumatic Line Insp. and Modification
JCAB AD TCD-6127-2003 26-dec-02
09-sep-03
MITSUBISHI SB
240
Inst.of Trottle Quadrant Placard 26-feb-03 02-jun-03
MITSUBISHI SB
241
A Inspection of Wing Attachment
Hardware
FAA, U.S AD 2006-13-15 JCAB AD TCD-
7030-2006
21-nov-
06
A 17-jan-07 c/o in conjunction with wingstudie
MITSUBISHI SL 060 System 17-feb-89 24-jul-91
MITSUBISHI SL 078 Automatic Autopilot Disconnect System
28-jan-02 07-Oct-2010
MITSUBISHI SL 079 Diode inst.in Flap Position Ind.Curcuit 28-jan-02 09-feb-01 Carried out by Mitsubishi (manufacturing-made)
MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02
26-aug-02 Compliance in according to HC-SB-61-256.
MITSUBISHI SL 084 Pneumatic De-Ice Monitoring System 14-jun-04 07-Oct-2010
MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-2005
14-sep-05
MITSUBISHI SN 053
B Rudder Torque Tube AD 86-20-01, SB 020/34-005
05-nov-86
B 26-Oct-1987
MITSUBISHI SN 117
D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD TCD-4753-98 LFV LVD2922
14-jun-04 D 11-dec-03
MITSUBISHI SN 146
Water Ingress into Vertical Stabilizer 19-dec-03
30-apr-04
MITSUBISHI SN 148
Reminders for safe operation 18-nov-05
22-mar-06 Genomförs enl. AMP MU-2 & DHB
MITSUBISHI SN
156A
Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered
MITSUBISHI SN
157
Torque Indicating System Shift
Potential
20-nov-
08
11-mar-09 SB 233 considered
MITSUBISHI SN
161
Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-
09
11-mar-10 Ref STC SA01913SE
MITSUBISHI SR
053A
Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-
2450A-87 LFV LVD2015 Rev B MAI SR 020/34-005 MITSUBISHI SB 223
23-Oct-
1984
12-May-1998
MITSUBISHI SR 064
Pitot & Static System MITSUBISHI SB 223 30-apr-85
15-feb-00
MITSUBISHI SR 065
Warning Horn 20-jan-86 13-Oct-1987
MITSUBISHI SR
067
Emergency Exit Placard 17-sep-
85
18-aug-87
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2012-12-06 ange ange
Dokumentnummer Sida
ange 193(195)
MITSUBISHI SR 072
Air Filter Replacement for Vacuum Syst.
25-apr-00
14-dec-01
MITSUBISHI SR
075
Inst. tip tank placard 29-Oct-
2004
29-apr-05
MITSUBISHI STC
SA01913SE
Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-
09
11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection
NARCO, Narco
NARCO SB ELT10-16
ELT ASSY 18-apr-88
19-jun-91 N/A
NYGE, Saab
Aerotech Aircraft
Services
NYGE TDM 00-18 Förstärkning av tidigare utförd skarv-
reparation kroppsida
19-Oct-
2000
27-Oct-2000 Reparation utförd
NYGE TDM 00-21 Domkraftskada 12-dec-
00
09-feb-01
NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00
25-jan-00
NYGE TDM 02-24 Installation Moving MAP 10-Oct-2002
18-dec-02
NYGE TDM 02-32 Installation EMI film 10-dec-02
10-jan-04
NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 install.
04-mar-03
8 16-Oct-2008
NYGE TDM 03-28 F Nav Demo Pod 19-dec-03
F 21-jan-10 Doubler/Grommet/Connector remain to install. Ref. defectlog No:869 Original compliance by Rev D. Not
affected by rev F.
NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05
18-nov-05
NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06
A 07-feb-08
NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07
A 07-feb-08
NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 28-feb-08
NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 07-sep-09
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Dokumentnummer Sida
ange 194(195)
NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08
B 16-Oct-2008 Original compliance with TDM rev A. Rev B does not affect previous complaiance.
NYGE TDM 09-32 A GPS Splitter 12-nov-
09
A 21-jan-10
NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 15-jun-10
NYGE TDM 10-03 A Pressure Bulkhead Feed Through 04-May-2010
A 15-jun-10
NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10
A 18-May-2010 C/W
NYGE TDM 11-35 A Terminating resistor 30-Jan-12
NYGE TDM 12-21 A Avinstalltion IK 14-Aug-12
NYGE TDM 95-04 4 Vingstudie 20-sep-98
31-mar-08
NYGE TDM 99-12 Avionic Modification SE-IUA 14-dec-99
07-feb-00
NYGE TVO 1/09 Inspektion av Stringers & struktur vinge
25-feb-09 02-mar-09 Inspected u/a
NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 08-apr-93
NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-
96
09-feb-00
NYGE TVO 1/97 3 De-Icertank MU-2B,
korrosionskontroll
12-feb-97 10-mar-97
NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01-dec-
00
09-feb-01
NYGE TVO 2/07 A Prevent FR31 radio to xmit when RM2 off
06-feb-07 A 02-mar-07
NYGE TVO 2/10 1 Visual inspection of center wing 19-apr-10
1 09-jul-10
NYGE TVO 2/91 A/C Elecrical System 10-jan-91 08-May-1992
NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06
07-Oct-2010
NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 01-jun-09
NYGE TVO 4/11 A Static inverter control 15-Dec-12
NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92
2 07-Oct-2010
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Dokumentnummer Sida
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NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 08-May-1992
NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92
09-nov-92
NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94
3 07-Oct-2010
NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning.
25-Oct-1996
19-aug-97 Utförd tidigare (ref. Ove N. lista)
NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 09-jul-10
NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-1992
09-nov-92
NYGE TVO 7/05 RMI-nål park. ej / ILS frekvens är vald 11-nov-05
01-nov-05
NYGE TVO 7/93 Starter Drive Splines 01-nov-93
16-nov-94
NYGE TVO 8/04 Kontr. av Spant vid bakre feninfästning
08-dec-04
30-nov-09
NYGE TVO 8/92 Wheel Parts 27-Oct-1992
08-apr-93
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