This document is posted to help you gain knowledge. Please leave a comment to let me know what you think about it! Share it to your friends and learn new things together.
Transcript
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
21-05 Environmental control system.- Do ageneral visual inspection of bolts that attach air Note 2 - This task is necessary all times you do a maintenance task in the areas where 125.- general visual inspection of bolts that attach airconditioning unit pylon to upper deck structure. 0B-A-21-91-03-00A-282A-A
13024-05 Electrical power system.- Do anOperational Check of DC Essential B s 1 Diode 03 Oct 07 0 0 0 0 0 0 0 354 6 2000 0 INSPECTION 2000 0 1645 4130.- Operational Check of DC Essential Bus 1 Diodefor open circuit failure. 0B-A-24-61-00-00A-320C-A
24-07 Electrical power system.- Do anOperational Check of Relay K7212 to verify thatthe contacts are not set to the emergency position.0B-A-24-61-00-00A-320D-A
25-01 Rescue hoist system.- Do an OperationalCheck of Rescue Hoist Intermediate Up and DownLimit Switches to confirm automatic speedreduction. 0B-A-25-91-00-00A-320A-A
25-02 Rescue hoist system.- Do an OperationalCheck of Rescue Hoist Full-Out and Full-In LimitSwitches to confirm all operations areautomatically stopped.0B-A-25-91-00-00A-320A-A
- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION Prior first use of day
Prior first use of day
automatically stopped.0B A 25 91 00 00A 320A A
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 6 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
25-03 Rescue hoist system.- Do a General VisualInspection of Rescue Hoist Cable Cutter Cotter Pinto ensure cotter pin is correctly installed. 0B-A-25-91-01-00A-281A-A
25 04 Rescue hoist system. Do an OperationalCheck of Rescue Hoist Cable Foul DetectionCircuit to ensure correct operation and that alloperations are automatically stopped. 0B-A-25-91-00-00A-320A-A
25-07 Rescue hoist system.- Following use in asalt water environment, wash complete cablelength and hook assembly with fresh water, anddry using a clean lint free cloth. 0B-A-25-91-01-00A-258A-A
25-08 Rescue hoist system.- Do an OperationalCheck of Cable Cut Switch to determine theexistence of dormant closed circuit failures of theswitch guard contact #2 and the push-buttoncontacts #1 and #2. 0B-A-25-91-00-00A-320B-A
26-01 Fire detection system.- Do a check ofpressure-transducer alarm-switch contacts fordormant open circuit failures and integrity switchcontacts for closed circuit failures. 0B-A-26-11-01-00A-340A-A
63-01 Rotor brake system.- Do a general visualinspection of rotor brake disc for damage andcondition. If you find that disc is damaged, replaceit. 0B-A-63-51-03-00A-282A-A
63-03 Rotor brake system. Verify that ROTORBRAKE ON warning and ROTOR BRK cautionmessages are correctly generated and shown oncockpit EDU. 0B-A-63-51-00-00A-320A-A
148.- 25-01 Rescue hoist 2000 lifts or 5 years. Use limitthat occurs first (Note 1) 109-0900-61-803 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 2000 5 YR RETIREMENT
149.- 25-02 Cargo hook 200-216-00 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT
150.- 25-03 Cargo hook 109-0705V03-107 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT
151.- 25-04 Safety cargo hook 528-010-01 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT
164.- 25-01 ELT battery pack. By F.A.R. 91.207 455-5049-345 A00057 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7165.- 25-02 First aid kit. Note 2 999-9001-02-105 UNK 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7166.- 25-03 Rescue hoist cable cutter cartridge BL-11140-1 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT
167.- 25-03 Rescue hoist cable cutter cartridge BL-11140-1 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 9 YR RETIREMENT CARTRIDGE FROM DATEOF MANUFACTURE
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE BY PART NUIMBET INSTALLED.
168.- 26-01 Portable fire extinguisher A072A02 01-2007/04998 31-Jan-07 0.0 0 0.0 NEW 354.6 - - - 10 YR RETIREMENT - - 30-Jan-17 - - 2435.0 FROM DATE OFMANUFACTURE
169.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 31-May-06 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 30-May-21 - - 4016.2 FROM DATE OFMANUFACTURE
170.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION
171.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 31-May-06 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 30-May-21 - - 4016.2 FROM DATE OFMANUFACTURE
172.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION
173.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 27-Feb-22 - - 4289.2 FROM DATE OFMANUFACTURE
174.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION
175.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 27-Feb-22 - - 4289.2 FROM DATE OFMANUFACTURE
176.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION
177.- 28-01 Fuel filter element KD651510 NOT APPLICABLE 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 1 YR RETIREMENT 700.0 - 25-Nov-10 345.4 - 176.7178.- 32-01 Snow ski restraint cables and bungee cords 109-0811-73-123 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT
179.- 32-01 Snow ski restraint cables and bungee cords 109-0811-73-125 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT
180.- 32-01 Snow ski restraint cables and bungee cords 109-0812-01-101 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT
181.- 32-01 Snow ski restraint cables and bungee cords 000-1034701/-02 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT
182.- 32-02 Slump pad bungee cords 109-0811-73-119 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT - - 02-Oct-10 - - 123.2183.- 32-02 Slump pad bungee cords 109-0811-73-121 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT - - 02-Oct-10 - - 123.2184.- 32-02 Slump pad bungee cords 109-0811-73-133 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT - - 02-Oct-10 - - 123.2185.- 62-01 Elastomeric bearing. Note 2 109-0111-04-101 LK1539 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7186.- 62-01 Elastomeric bearing. Note 2 109-0111-04-101 LK1542 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7
CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-41-00-00A-000A-A Standard inspection program
218.- 00-01 Obey with the requirements for inspectionsof optional equipment. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION
219.-
24-01 Starter-generators. Examine brushes (onlyif APC standard or XL brushes are installed) forwear. Examine commutator contacts for wear,pitting and burnings.
CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-44-00-00A-000A-A Special inspections
Obey with the requirements for inspections of optional equipment.
220.-
24-01 Starter-generators. Examine brushes (onlyif APC standard or XL brushes are installed) forwear. Examine commutator contacts for wear,pitting and burnings.
t l d i h ft f (h d li P/N 109 0760 42 103 BH303 03 O t 07 0 0 0 0 0 NEW 354 6 1600 0 1600 0 1245 4222.- external drive shafts for wear (hydraulic pump P/N109-0760-42-103 only).
223.-32-01 Landing gear actuators (helicopters whichoperate over sea and/or in high humidity),Examine for corrosion and damage.
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 900.0 - 3 YR INSPECTION 900.0 - 02-Oct-10 545.4 - 123.2
224.-32-02 Landing gear actuators (helicopters whichdo not operate over sea and/or in high humidity)Examine for corrosion and damage.
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1800.0 - 6 YR INSPECTION 1800.0 - 02-Oct-13 1445.4 - 1219.0
225.-
62-01 Main rotor dampers Examine for conditionand unusual play of bearings. Note 2.- 2 Only ifyou apply the extended and progressive inspectionprograms.
235.-62-05 Main rotor blades (removal necessary) Examine bladeand its bushings for wear, nicks and conditions. Examinecontact areas with grips for condition.
236.- 62-06 Main rotor head control levers (removal necessary)Examine for condition, damage and wear. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -
62 07 M i t bl d i ( l ) E i
CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-44-00-00A-000A-A Special inspections
237.-62-07 Main rotor blade grips (removal necessary) Examinefor condition, damage and wear. Examine contact areas withblades for condition and washer bondage.
239.- 62-09 Main rotor head and installation components (removalnecessary) Do a detailed examination. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -
240.- 62-10 Hub floating ring Examine for wear. Examine DUwashers and internal Teflon shim for debonding - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -washers and internal Teflon shim for debonding.
241.-62-11 Swashplate (removal and disassembly necessary)Examine duplex bearing for damage and corrosion. Examineteflon rings for wear. Examine swashplate guides and pivotsleeve slots for damage and wear.
246.- 64-01 Tail rotor Do a check for correct dynamic balance. - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -
247.-64-02 Blade elastomeric bushings and related hub contactareas (blade removal necessary) Examine for condition,fretting and wear. Note 3.- Only if you apply the standardinspection program.
256.- 32-03 Main landing gear struts (2 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR Fill with nitrogen - - 25-Nov-10 - - 176.7257.- 32-03 Main landing gear struts (2 off) - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - Fill with fluid 1600.0 - - 1245.4 - -258.- 32-04 Nose landing gear strut - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR Fill with nitrogen - - 25-Nov-10 - - 176.7259.- 32-04 Nose landing gear strut - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - Fill with fluid 1600.0 - - 1245.4 - -260.- 32-05 Landing gear wheel tires (3 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Fill with nitrogen 500.0 - 25-Nov-10 145.4 - 176.7
261.- 32-06 Wheel bearings (Note 2.- Only when the helicopteroperates in salt laden atmosphere. ) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR Grease - - 25-Nov-10 - - 176.7
262.- 62-01 Main rotor blade (4 off) (Note 2.- Only when thehelicopter operates in salt laden atmosphere. ) - - 11-Mar-08 99.5 446 0.0 NEW 255.1 - - - 7 DAYS Apply surface protection Note 2.- Only when the helicopter operates in salt laden atmosphere.
263.- 62-02 Main rotor floating ring and droop stop plates - - 17-Mar-10 341.5 1177 0.0 -8.5 13.1 - 50.0 - 3 MO Grease 400.0 - 16-Jun-10 45.4 - 14.8
272.- 71-01 Engines (2 off) Note 3. Refer to the enginemaintenance manual for the oil change interval. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - Change of oil Note 3. Refer to the engine maintenance manual for the oil change interval.
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 12 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
273.- 00-01 Obey with the requirements for inspectionsof optional equipment. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION
274.-
18-01 Vibration absorber-to-fuselage attachmentbolts, Examine for correct torque. (Note 1 If youfound that the torque is not in the approved limits,do a torque check again after 5 thru 10 hours offlight ) 5 thru 10 hours of flight when the
- - 10-Sep-07 8.3 8 0.0 NEW 346.3 - 10.0 - - INSPECTION COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.
CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )
Obey with the requirements for inspections of optional equipment.
CHAPTER 0B-A-05-51-00-00A-000A-A Out of phase inspections – General
flight.) 5 thru 10 hours of flight, when thehelicopter is new, or after the installation of avibration absorber.
53-01 Tail boom attachment bolts Examine forcorrect torque. (Note 1 If you found that the torque
At each removal of a cockpit door.
After each removal of a wheel tire.
277.- is not in the approved limits, do a torque checkagain after 5 thru 10 hours of flight.) 5 thru 10hours of flight, when the helicopter is new, or afterthe installation of the tail boom.
COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.
Before the first flight of a day.
279.-
62-02 Main rotor head ring nut bolts Examine forcorrect torque. (Note 1 If you found that the torqueis not in the approved limits, do a torque checkagain after 5 thru 10 hours of flight.) 5 thru 10hours of flight, when the helicopter is new, or afterthe installation of the main rotor.
COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.
281.-
63-01 Upper cover-to-main case attachment nutsExamine for correct torque. (Note 1 If you foundthat the torque is not in the approved limits, do atorque check again after 5 thru 10 hours of flight.)5 thru 10 hours of flight, when the helicopter isnew, or after the installation of the maintransmission.
282.- 63-02 Fan pulleys Examine for condition,damage and wear. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION
283 63-03 Fan bearings Examine for excessive play 03 Oct 07 0 0 0 0 0 NEW 354 6 INSPECTION
COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.
After each removal of a fan belt
After each removal of a fan belt.
283.- g p yand roughness. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION
284.-
65-01 Mounting sleeve attachment bolts Examinefor correct torque. (Note 1 If you found that thetorque is not in the approved limits, do a torquecheck again after 5 thru 10 hours of flight.) 5 thru10 hours of flight, when the helicopter is new, orafter the installation of the 90-degree gearbox.
71-01 Exhaust ejector-to-saddle attachmentbolts Examine for correct torque. (Note 1 If youfound that the torque is not in the approved limits,do a torque check again after 5 thru 10 hours offlight.) 5 thru 10 hours of flight, when thehelicopter is new, or after the installation of anengine exhaust ejector.
- - 10-Sep-07 8.3 8 0.0 NEW 346.3 - 10.0 - - INSPECTION COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.
CHAPTER 0B-A-05-51-00-00A-000A-A Out of phase inspections – GeneralCHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )
299.- Rotor brake control cable Do operation test. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
300.- Rotor brake control cable Do operation test. PIP - 12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 14 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
302.- Bleed air lines, pipes, joints and fittings. Examinefor condition and security. EIP - 200 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION
303 Bleed air lines, pipes, joints and fittings. Examine 03 Oct 07 0 0 0 0 0 NEW 354 6 200 0 INSPECTION
CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE AIRCRAFT IN STANDAR PROGRAM
CHAPTER 0B-A-05-70-02-00A-000A-A Scheduled/unscheduled inspections - Environmental control system
303.- , p p , j gfor condition and security. PIP - 200 hours - PH C - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION
304.- Bleed air overtemperature switch. Do function test.SIP - 100 hours - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -
305.- Bleed air overtemperature switch. Do function test.EIP - 200 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION
306.- Bleed air overtemperature switch. Do function test.PIP - 200 hours - PH C - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION
307.- Environmental control system. Do operation test. SIP - 12months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
308.- Environmental control system. Do operation test. EIP - 12months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
309.- Environmental control system. Do operation test. PIP - 12months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
310.-
Heat exchanger Do detailed examination SI - 400hours (Note 1.- Only after the first 400 hours ofoperations. Subsequently do the inspection at 200hours interval.)
Bottles. Do hydrostatic test SI - 5 years (Note 1.- To do thehydrostatic test, refer to the instructions printed on the decalsof the bottles. The bottles must be removed from thehelicopter. Refer to 0B-A-26-21-01-00A-520A-A and 0B-A-26-22-01-00A-520A-A.)
27300-1 1042 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 5 YR HYDROSTATIC TEST - - 28-Feb-12 - - 636.7
342.-
Bottles. Do hydrostatic test SI - 5 years (Note 1.- To do thehydrostatic test, refer to the instructions printed on the decalsof the bottles. The bottles must be removed from thehelicopter. Refer to 0B-A-26-21-01-00A-520A-A and 0B-A-26-22-01-00A-520A-A.)
27300-1 1046 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 5 YR HYDROSTATIC TEST - - 28-Feb-12 - - 636.7
343.-Bottles. Do operation test of discharge heads tomake sure that they operate when necessary. SI -10000 h
344.-Bottles. Do operation test of discharge heads tomake sure that they operate when necessary. SI -10000 h
27300-1 1046 03-Oct-07 0.0 0 0.0 NEW 354.6 - 10000.0 - - INSPECTION 10000.0 - - 9645.4 - -10000 h
345.- FIRE EXT circuit breakers. Do operation test fordormant open circuit failures. SI - 10000 h - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 10000.0 - - INSPECTION 10000.0 - - 9645.4 - -
346.-
Fire extinguisher control panel. Do operation testof BTL switch and ENG 1 and ENG 2 lighted push-button switches for open circuit failures. This tomake sure that they operate when necessary. SI -10000 h
357.-Hoist motor and cable cutter electricalconnections. Examine for condition and security.EIP - 50 hours / 30 days
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
358.-Hoist motor and cable cutter electricalconnections. Examine for condition and security.PIP - 50 hours / 30 days
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
359.-
Hoist hook and spring bumper. Examine to makesure that hook is safety homed and spring bumpersufficiently compressed. This to present hookmovement when helicopter is in flight. SIP -Airworthiness check
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
Airworthiness check
360.-
Hoist hook and spring bumper. Examine to makesure that hook is safety homed and spring bumpersufficiently compressed. This to present hookmovement when helicopter is in flight. EIP - 50hours / 30 days
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
361 -
Hoist hook and spring bumper. Examine to makesure that hook is safety homed and spring bumpersufficiently compressed This to present hook - - 03-Oct-07 0 0 0 0 0 NEW 354 6 - 50 0 - 30 DAYS INSPECTION
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.361.- sufficiently compressed. This to present hookmovement when helicopter is in flight. PIP - 50hours / 30 days
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
383.- Rescue hoist installation Do a detailed inspection. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION
384.- Cable swaged ball end. Examine for security of attachment. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION
385.-Hoist hook assembly. Examine for defect,corrosion and binding. OPI - Every month, 25 liftsor 50 flight hours. Use limit that occurs first (Note 1)
OPI - After last flight of the day (if hoist used)
OPI - After last flight of the day (if hoist is used)
g ( )
386.-
Hoist cable. Examine for defect. Make sure thatcable is correctly wound on drum. OPI - Everymonth, 25 lifts or 50 flight hours. Use limit thatoccurs first (Note 1)
387.-Hoist tension roller. Examine for wear and defects.OPI - Every 6 months, 400 lifts or 100 flight hours.Use limit that occurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
388.-
Hoist tension roller and overrunning clutchassemblies. Examine for correct operation andwear. OPI - Every 6 months, 400 lifts or 100 flighthours. Use limit that occurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION
389.-Hoist cable guide. Examine for wear. OPI - Every 6 months, 400 lifts or 100 flight hours. Use limit thatoccurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION
390Hoist chain. Examine for correct tension. OPI -E 6 th 400 lift 100 fli ht h U 03 O t 07 0 0 0 0 0 NEW 354 6 100 0 400 6 MO S C O
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE EQUIPMENT NOT INSTALLED
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
390.- Every 6 months, 400 lifts or 100 flight hours. Uselimit that occurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION
391.-Hoist pressure rollers. Examine for corrosion andwear. OPI - Every 6 months, 400 lifts or 100 flighthours. Use limit that occurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION
392.-Hoist level wind shaft and follower. Examine forwear. OPI - Every 6 months, 400 lifts or 100 flighthours. Use limit that occurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
393.-Hoist. Examine for correct oil level. OPI - Every 6months, 400 lifts or 100 flight hours. Use limit thatoccurs first (Note 1)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION
394.- Hoist, hook and cable. Wash. OPI - Every month - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 MO INSPECTION
395.- Rescue hoist installation. Do an operation test.OPI - Every 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 19 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
409.- Rear view mirror. Examine for condition andsecurity. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
410.- Rear view mirror. Examine for condition andsecurity. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
411.- Cargo hook support frame, supports and adjacent fuselageareas. Examine for corrosion and damage. SIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
412.- Cargo hook support frame, supports and adjacent fuselageareas. Examine for corrosion and damage. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
413.-Cargo hook support frame, supports and adjacent fuselageareas. Examine for corrosion and damage. PIP - 12 months -PH I
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
414.-Safety cargo hook crossbeam, supports and adjacentfuselage areas. Examine for corrosion and damage. SIP - 12months
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
415.-Safety cargo hook crossbeam, supports and adjacentfuselage areas. Examine for corrosion and damage. EIP - 12months
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 20 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
419.- Cargo hook load measuring system. Do operation test. PIP -12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
420.-Cargo hook. Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hookand send it to the Manufacturer fro overhaul.). SIP - 12 months
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
421.-Cargo hook. Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hook - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
y p gand send it to the Manufacturer fro overhaul.). EIP - 12 months
422.-
Cargo hook. Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hookand send it to the Manufacturer fro overhaul.). PIP - 12months - PH I
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
423.-
Safety cargo hook. Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargoh k d d it t th M f t f h l ) SIP 12
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.hook and send it to the Manufacturer fro overhaul.). SIP - 12months
424.-
Safety cargo hook. Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargohook and send it to the Manufacturer fro overhaul.). EIP - 12months
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
425.-
Safety cargo hook. Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargo - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.425. 1. If you find corrosion on the side plates, remove the cargohook and send it to the Manufacturer fro overhaul.). PIP - 12months - PH I
03 Oct 07 0.0 0 0.0 NEW 354.6 1 YR INSPECTION
426.-
Cargo hook Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hookand send it to the Manufacturer fro overhaul.). SI - Everymonth (if cargo hook is used or is stored in a marineatmosphere)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 MO INSPECTION
Safet cargo hook E amine e ternal s rfaces for corrosion
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
427.-
Safety cargo hook Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargohook and send it to the Manufacturer fro overhaul.). SI - Everymonth (if cargo hook is used or is stored in a marineatmosphere)
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 MO INSPECTION
428.-Cargo hook installation. Do operation test ofisolation relays for closed circuit failures. SI - 2000hours
430.- Upper cutter. Examine for condition and security.SIP - Airworthiness check - - 08-Dec-08 193.6 716 0.0 NEW 161.0 - 100.0 - - INSPECTION
431.- Upper cutter. Examine for condition and security.EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
432.- Upper cutter. Examine for condition and security.PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
N tt E i f diti d l k d i
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
CHAPTER 0B-A-05-70-09-00A-000A-A Scheduled/unscheduled inspections - Wire strike protection system CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )
433.-
Nose cutter Examine for condition and locked inforward tilted position [1 CAUTION: Damage mayresult from landing gear retraction if the nosecutter is not locked in forward tilted position.] SIP -100 hours
Nose cutter Examine for condition and locked inforward tilted position [1 CAUTION: Damage mayresult from landing gear retraction if the nosecutter is not locked in forward tilted position.] EIP -200 hours
Nose cutter Examine for condition and locked inforward tilted position [1 CAUTION: Damage mayresult from landing gear retraction if the nosecutter is not locked in forward tilted position.] PIP -200 hours - PH C
444.-Fittings, restraint cables and bungee cords.Examine for damage and security. PIP - 50 hours /30 days
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
445.- Restraint cables. Examine for corrosion. OPI - 12months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
446.-
Snow skis. Examine for deformation. Payparticular attention to any permanent deformationto the cable supports (sheet metal parts),especially to any sheet metal layer separation inthe cable attachment area. OPI - 12 months
- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
447.-
Snow skis. Examine for deformation. Payparticular attention to any permanent deformationto the cable supports (sheet metal parts),especially to any sheet metal layer separation inthe cable attachment area. CI - Hard landing
NOT APPLICABLE, EQUIPMENT NOT INSTALLED.security. SIP - Airworthiness check
452.- Bungee cords support. Examine for distortions andsecurity. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
453.- Bungee cords support. Examine for distortions andsecurity. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION
1. Visual inspection.Note 1 Refer to Maintenance Planning
CH 0B-A-20-60-01-00A-289A-A Corrosion control – Inspection of corrosion damage
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.
454.-
Note 1.- Refer to Maintenance PlanningInformation publication (0B-A-AMPI-00-P) fordetailed inspection and preventive maintenancerequirements. Note 2.- These inspections should beaccomplished in conjunction with other requiredpreventive maintenance.
461 RATE GYRO 7007453 902 06121572 03 Oct 07 0 0 0 0 0 NEW 354 6 ON CONDITION REPLACEMENT
CHAPTER 22 AUTO FLIGHT "ON CONDITION"ON CONDITION
CHAPTER 21 AIR CONDITIONING "ON CONDITION"ON CONDITION
ON CONDITION
ON CONDITION COMPONENTS
ON CONDITION
461.- RATE GYRO 7007453-902 06121572 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
462.- AIR DATA SENSOR D60350MK211212 000774-005 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
463.- F/D CONTROL PANEL 7000605-901 06123354 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
464.- HRLIPILOT ACTUATOR ASSY 109-0020-86-1 0611H688 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
465.- HRLIPILOT ACTUATOR ASSY 109-0020-86-1 0611H686 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
466.- HRLIPILOT ACTUATOR ASSY 109-0020-86-3 0612H778 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
467.- HRLIPILOT ACTUATOR ASSY 109-0020-86-3 0612H772 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
468.- HRLIPILOT ACTUATOR ASSY 109-0040-55-3 0612H806 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
469.- SAS/FD CONTROL PANEL 109-0729-49-1 938 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
470.- F/D COMPUTER (TYPE FZ-702) 109-0900-56-101 0346 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
471 HELIPILOT COMPUTER N 1 (TYPE SP711) 109 0900 64 103 0761 03 O t 07 0 0 0 0 0 NEW 354 6 ON CONDITION
ON CONDITIONON CONDITION
ON CONDITIONON CONDITION
ON CONDITION
ON CONDITION
ON CONDITION
ON CONDITION
ON CONDITION
ON CONDITION
ON CONDITION
471.- HELIPILOT COMPUTER N.1 (TYPE SP711) 109-0900-64-103 0761 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
472.- HELIPILOT COMPUTER N.2 (TYPE SP711) 109-0900-64-103 0914 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
473.- VHF ANTENNA N.1 VFS 10-90-2 6134 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
474.- VHF ANTENNA N.2 VFS 10-90-2 6212 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
475.- ICS AMPLIFIER 251-002 1394 14-Jan-08 211.3 764 0.0 REP 143.3 - ON CONDITION - REPLACEMENT S/N 1567 OFF
476.- GNS 530 RECEIVER 010-00182-10 78417645 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
477.- GNS 430 COMM/NAV GPS UNIT CPLT 010-00139-10 011-0028-10
97139635 97139629 13-Mar-09 UNK UNK 0.0 OVH #¡VALOR! - ON CONDITION - REPLACEMENT SAME PART
NSTALLEDON CONDITION
ON CONDITION
ON CONDITIONON CONDITIONON CONDITIONON CONDITION
ON CONDITION
CHAPTER 23 COMMUNICATIONS "ON CONDITION"
ON CONDITION
478.- ICS CONTROL PANEL CPLT AA95-954TSO 2045 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
479.- ICS CONTROL PANEL PLT AA95-954TSO 2046 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
480.- CABIN AUDIO PANEL AA82-060 2153 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
481.- ICS CONTROL PANEL AA31-002 2417 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
482.- MAIN BATTERY 2778-1 S00615 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
483.- DC CONTROL BOX N.1 GCSG505-28-1 2254D 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
484.- DC CONTROL BOX N.2 GCSG505-28-1 2257D 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
485.- INVERTER N.1 PC 251A 26140 25-Jun-08 136.7 532 0.0 NEW 217.9 - ON CONDITION - REPLACEMENT S/N 25018 OFF
486.- INVERTER N.2 PC 251A 25101 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
ON CONDITIONON CONDITIONON CONDITION
ON CONDITION
CHAPTER 24 ELECTRICAL POWER "ON CONDITION"ON CONDITIONON CONDITION
ON CONDITIONON CONDITIONON CONDITION
486. INVERTER N.2 PC 251A 25101 03 Oct 07 0.0 0 0.0 NEW 354.6 ON CONDITION487.- DC ELECTRICAL BOX 109-0729-99-101 N367 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
488.- DETECTRO BOX 109-0900-19-101 90 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT
LH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The methodused to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).
LH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The method
d t t d it th i i t th di ti f th O t
PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 1750.0 - - HOT SECTION INSPECTIONON CONDITION, from the results of the power assurance check or the engine health trend
monitoring.
used to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).
658.- LH ENGINE; POWER ASSURANCE CHECKS,Less than 175 hours CH. 71-00-00 PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - 100.0 - - HOT SECTION INSPECTION 400.0 - - 45.4 - - EFECTUAR POR LA
y g ( ) g ( )Every 40 to 50 hours, the operators must enter theaccumulated cycles for each LCF component inthe engine logbook. This data is obtained eitherfrom the helicopter display system or directly fromthe DCU using the Ground Base Software (GBS)program.
LH (PW206C) Hot Section.- Compressor TurbineBlades (Pre-SB28069); Do a borescope inspectionof the compressor turbine blades for evidence ofblade shifting (Ref. 72-00-00, Engine, General -Inspection)
LH (PW206C) Hot Section.- Power TurbineBlades (Pre-SB28187 or Pre-SB28239); Do aborescope inspection of the power turbine bladesfor evidence of blade shifting (Ref. 72-00-00,Engine, General - Inspection)
LH Engine Externals.- Connectors of the ElectricalWiring Harness; Do a security check to verifyconnector security. Apply enhancer, electricalcontact (PWC05-256) to the speed/torqueconnectors P7, P9, P10 and sensors.0, (Ref. 73-21-40, ELECTRICALWIRING HARNESS - MAINTENANCEPRACTICES).
g g ;Do a general visual check on the wires forevidence of chafing, cracks, corrosion and wear.Also verify if the nuts of the terminal junction aresecured. Do a heat response check on eachindividual probe. (Ref. 77-21-00, MGT SENSORSAND TRIM UNITS - INSPECTION/CHECK)
LH Engine Externals.- Air Inlet Screen; Do a visualcheck of the screen for blockage, damage and thatthe attaching hardware is serviceable (72-21-00,AIR INLET - INSPECTION/CHECK).
LH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):
PW207CNew heat shield:
Every 25 hours for the first 50 hours
30-Jul-07 0.0 0 0.0 NEW 354.6 - 25.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.
689.-
LH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):
LH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):
PW207C Heat shield: with acceptable cracks 30-Jul-07 0.0 0 0.0 NEW 354.6 - 10.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.
NOT APPLICABLE BY ENGINE MODEL.
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 30 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
LH Fuel.- Fuel Nozzles; Clean and do a functionalcheck of the fuel nozzles (Ref. CMM 3040870).Inspect the fuel nozzle inlet screens. Ifcontamination is found, follow the Fuel ImpendingBy-Pass Indicator Activated fault isolation chart (Ref. 72-00-00).
LH (PW206C) Fuel.- Fuel Accumulator (Pre-SB28164); A general visual check for a bellowsfailure indication (through the pop-out indicator). If PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.an indication is present, replace the fuelaccumulator.
697.-LH Ignition.- Igniter Plug; Do a detailed visualcheck of the igniter plug for erosion (Ref. 74-11-00, ENGINE IGNITION - INSPECTION/CHECKS).
. PRATT & WHITNEY PE207C ENGINE 1 S/N PCE-BH0141 ; AIRWORTHINESS LIMITATIONS ISSUED DATE May 08/2009
. TABLE 2, PW207C Engines, Part Numbers for Automatic Life Cycle Counting709.- Data Collection Unit 3054276-01 - 30-Jul-07 0.0 0 0 NEW 548 - - - - REPLACEMENT
710.- Data Collection Unit (Post-SB28273) 3054276-02 - 30-Jul-07 0.0 0 0 NEW 548 - - - - REPLACEMENT
RH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The methodused to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).
RH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The method
PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 0.0 354.6 - 1750.0 - - HOT SECTION INSPECTIONON CONDITION, from the results of the power assurance check or the engine health trend
monitoring.paper, and trend the data to monitor the engines health. The methodused to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).
722.- RH ENGINE; POWER ASSURANCE CHECKS, Less than 175 hours CH. 71-00-00 PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - 100.0 - - HOT SECTION INSPECTION 400.0 - - 45.4 - - EFECTUAR POR LA
Automatic Low Cycle Fatigue (LCF) Counting. (4)Every 40 to 50 hours, the operators must enter theaccumulated cycles for each LCF component inthe engine logbook. This data is obtained eitherfrom the helicopter display system or directly fromthe DCU using the Ground Base Software (GBS)program.
RH (PW206C) Hot Section.- Compressor TurbineBlades (Pre-SB28069); Do a borescope inspectionof the compressor turbine blades for evidence ofblade shifting (Ref. 72-00-00, Engine, General -Inspection)
RH (PW206C) Hot Section.- Power TurbineBlades (Pre-SB28187 or Pre-SB28239); Do aborescope inspection of the power turbine bladesfor evidence of blade shifting (Ref. 72-00-00,Engine, General - Inspection)
LH Engine Externals.- Connectors of the ElectricalWiring Harness; Do a security check to verifyconnector security. Apply enhancer, electricalcontact (PWC05-256) to the speed/torqueconnectors P7, P9, P10 and sensors.0, (Ref. 73-21-40, ELECTRICALWIRING HARNESS - MAINTENANCEPRACTICES).
g g ;Do a general visual check on the wires forevidence of chafing, cracks, corrosion and wear.Also verify if the nuts of the terminal junction aresecured. Do a heat response check on eachindividual probe. (Ref. 77-21-00, MGT SENSORSAND TRIM UNITS - INSPECTION/CHECK)
RH Engine Externals.- Air Inlet Screen; Do a visualcheck of the screen for blockage, damage and thatthe attaching hardware is serviceable (72-21-00,AIR INLET - INSPECTION/CHECK).
RH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):
PW207CNew heat shield:
Every 25 hours for the first 50 hours
30-Jul-07 0.0 0 0.0 NEW 354.6 - 25.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.
753.-
RH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):
RH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):
PW207C Heat shield: with acceptable cracks 30-Jul-07 0.0 0 0.0 NEW 354.6 - 10.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.
NOT APPLICABLE BY ENGINE MODEL.
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 35 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
RH Fuel.- Fuel Nozzles; Clean and do a functionalcheck of the fuel nozzles (Ref. CMM 3040870).Inspect the fuel nozzle inlet screens. Ifcontamination is found, follow the Fuel ImpendingBy-Pass Indicator Activated fault isolation chart (Ref. 72-00-00).
RH (PW206C) Fuel.- Fuel Accumulator (Pre-SB28164); A general visual check for a bellowsfailure indication (through the pop-out indicator). If PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.an indication is present, replace the fuelaccumulator.
761.-RH Ignition.- Igniter Plug; Do a detailed visualcheck of the igniter plug for erosion (Ref. 74-11-00, ENGINE IGNITION - INSPECTION/CHECKS).
RH Power Management. EEC/Fuel ManagementModule; Do a manual mode response check anddo an operational check of the alternate engineshutdown system. (Ref. applicable aircraft manual).
. PRATT & WHITNEY PE207C ENGINE 2 S/N PCE-BH0128; AIRWORTHINESS LIMITATIONS ISSUED DATE May 08/2009
. TABLE 2, PW207C Engines, Part Numbers for Automatic Life Cycle Counting773.- Data Collection Unit 3054276-01 - 03-Oct-07 0.0 0 0 NEW 548 - - - - REPLACEMENT
774.- Data Collection Unit (Post-SB28273) 3054276-02 - 03-Oct-07 0.0 0 0 NEW 548 - - - - REPLACEMENT
SB Number or Once orAD Number. Recurr Hrs Date Hrs Date Hrs Date Hrs Date
781.- BT-109S-26 MANDATORY 17-Apr-09 Once - 28-Feb-10 - -93.5
782.- BT-109S-31 MANDATORY 3-Aug-09 Once - 30-Sep-10 - 120.5 EN PROCESO WO#12300.1.2
APLICAR, INSTALADO N/P 109-0162-01-101 N/S P200547. REWORK OF THE TAIL ROTOR HUB AND BLADES ASSY P/N 109-0162-01-101. Within and not later than September 30, 2010.
Issue Date DescriptionTime Remaining
. AMENDMENTDate/Time Next Due
Metodo de CumplimientoInterval
NOTES &OBSERVATIONS
AIRWORTHINESS DIRECTIVES AND SERVICE BULLETINS
TAIL ROTOR CONTROL ROD ASSY P/N 109-0032-14-105 "UNA TANTUM" (ONE TIME) INSPECTION FOR INTERFERENCE AND LEFT SIDE TUBES INSTALLATION P/N 109-0322-11-401 REWORK BY THE APPLICATION OF THE KIT P/N 109-0824-43-101.
PART II^: Within and not later than February 28, 2010. APLICAR PARTE II
783.- BT-109S-34 MANDATORY 16-Nov-09 Once - 30-Sep-10 - 120.5
APLICAR HAY GARANTIAREPLACEMENT OF THE EFIS P/N 109-0900-71-1A01 OR -2A01 (ASTRONAUTICS P/N 193850-1, -3, -101 AND -103). Within and not later than September 30, 2010.
APLICAR HAY GARANTIAMODIFICATION OF THE “BATT BUS” CIRCUIT BREAKER INSTALLATION.
REPLACEMENT OF THE FLIGHT DIRECTOR COMPUTER, BY MEANS OF THE APPLICATION OF KIT P/N 109-0824-44-101.
REPLACEMENT OF THE HELIPILOT COMPUTERS, BY MEANS OF THE APPLICATION OF
HELICOPTERS AFFECTED: The Agusta A109S helicopters up to S/N 22151 included. COMPLIANCE: At Operator’s option.APLICAR.
APLICAR, NO HAYGARANTIA.
HELICOPTERS AFFECTED: All Agusta A109S helicopters up to S/N 22151 included. COMPLIANCE: At Operator’s option. APLICAR, NO HAY786.- BT-109S-36 OPTIONAL 26-Apr-10 Once - - -
787.- SAIB SW-08-03 R2 RECOMMENDED 15-Jan-10 Once
788.- SAIB CE-10-11 R1 RECOMMENDED 14-Jan-10 Once
Recommendations for Rotorcraft During Icing Conditions
We highly recommend and strongly urge you to perform the following: • Review the aircraft Flight Manual for Limitations and Operations guidance in falling/blowing snow and/or icing. Many aircraft are prohibited from operating in known icing and/or falling and blowing snow. •
Perform basic airmanship and preflight by evaluating current and predicted weather briefings from the area Flight Service Station. AGREGAR UNA COPIA PARA LOS PILOTOS.
AGREGAR UNA COPIA PARA LOSPILOTOS.
Electrical: Fire Hazard in Resetting Circuit Breakers (C/Bs)
RECOMMENDED, The rules, either CAR 3, § 3.691 or 14 CFR § 23.1357, require the C/Bs that are essential for safety in flight be located and marked so they can be reset in flight. The rules do not require segregation of non-essential C/Bs. This SAIB references the most current “best
practices” for circuit breakers, the electrical system and aging wiring. It is important to note that many older aircraft may have little or no guidance on resetting policy in their airplane flight manuals AGREGAR UNA COPIA PARA LOS PILOTOS
AGREGAR UNA COPIA PARA LOSPILOTOS.
KITS P/N 109-0824-45-101 AND -103. APLICAR. GARANTIA.
789.- AD2010-04-16 39-16209 8-Mar-10 Once - Mar-10 - 3 MO - - 7-Jun-10 - 5.8
790.- SAIB CE-10-22 RECOMMENDED 26-Mar-10 Once
guidance on resetting policy in their airplane flight manuals. AGREGAR UNA COPIA PARA LOS PILOTOS.
This SAIB advises you of an airworthiness concern regarding all modification levels of Honeywell GNS Series Navigation Systems: GNS_XLS PRNAV, part number (P/N) 17960-0103-XXX; GNS_XLS Enhanced PRNAV, P/N 17960-0204-XXX; and GNS_XL PRNAV, P/N 18355-0102-0XXX.
Recommendations, After reviewing the above data, we recommend that you adhere steps in page 1. VERIFICAR POR EQUIPO INSTALADO. VERIFICAR POR EQUIPOINSTALADO.
AD applies to Type H1-10 AIR Halon 1211 (BCF) portable fire extinguishers manufactured by SICLI, having part number (P/N) 1708337B4 and having any serial number listed in Table 1 of this AD.
VERIFICAR POR EQUIPOINSTALADO.
791.- AD2010-07-02 39-16246 3-May-10 Once - May-10 - 30 MO - - 1-Nov-12 - 883.6
TURBOSHAFT ENGINE COMPRESSOR DISC INSPECTION OF AND RETAINING NUT REPLACEMENT "ENGINE LH & RH"
CERTIFICAR, NO APLICA PORNUMERO DE SERIE DE LOS MOTOR.LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
AD applies to Honeywell Primus II RNZ-850( )/-851( ) INUs installed on any aircraft, regardless of whether the aircraft has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD.
VERIFICAR POR EQUIPOINSTALADO.
Effectivity PW207C Engines.. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR.TURBOSHAFT ENGINE CENTRIFUGAL IMPELLER - REPLACEMENT OF LH & RH APLICAR NO HAYGARANTIA
Effectivity PW206C Engines which are before and include Serial No. PCE-BC0611, PW207C Engines which are before and include Serial No. PCE-BH0068. CATEGORY 5 - P&WC recommends to do this service bulletin when the engine is disassembled and access is available to the
necessary subassembly (i.e. module, accessories, components, or build groups). Do all spare subassemblies. CERTIFICAR, NO APLICA POR NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
CERTIFICAR, NO APLICA PORNUMERO DE SERIE DE LOS MOTOR.LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
GARANTIA
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.
G.M.J.P. 38 de 39
REG. NUMBER / MATRICULA: XA-UIR
MANUFACTREDATE / FECHAFABRICACION:
03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0
MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.
CYCLES SINCE NEW C.S.N.
CYCLES SINCE OVERHAUL C.S.O. 0
Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life
HOURS ALLOWED / HORAS PROMEDIO
EXTERNAL HOIST CYCLES
OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.
SB Number or Once orAD Number. Recurr Hrs Date Hrs Date Hrs Date Hrs Date
795.- P&WC S.B. No. 28301 R3 CATEGORY 5 5-Feb-10 Once
AIRWORTHINESS DIRECTIVES AND SERVICE BULLETINSNOTES &OBSERVATIONS. AMENDMENT Issue Date Description
Date/Time Interval
Effectivity PW206C Engines which are before and include Serial No. PCE-BC0763. PW207C Engines which are before and include Serial No. PCE-BH0281 and Serial No. PCE-BH0283 thru Serial No. PCE-BH0305.CATEGORY 5 - P&WC recommends to do this service bulletin when
the engine is disassembled and access is available to the necessary subassembly (i.e. module, accessories, components, or build groups). Do all spare subassemblies. CERTIFICAR, PCW SB28301 R2, JAN-23-2010, AT A/CT T.T. 318:30 HRS & 756 CYC BY PHOENIX ENGINE
SERVICE WO# 1081 AP 214769163 JONNIE B. SMITH.
CERTIFICAR, PCW JAN-23-2010, ATA/CT T.T. 318:30 HRS & 756 CYC BYPHOENIX ENGINE SERVICE WO# 1081AP 214769163 JONNIE B. SMITH.
796.- P&WC S.B. No. 28303 R3 CATEGORY 7 4-Feb-10 Once
797.- P&WC S.B. No. 28305 R1 CATEGORY 7 8-Mar-10 OnceTURBOSHAFT ENGINE COMPRESSOR IMPELLER AND HOUSING SET - REPLACEMENT/MODIFICATION OF "ENGINE LH & RH"
Effectivity PW207C Engines which are before and include Serial No. PCE-BH0479. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
APLICAR, NUMERO DE SERIE DE LOSMOTOR. LH S/N PCE-BH-0141, RH S/NPCE-BH-0128.
Effectivity: PW206C Engines which are before and include Serial No PCE BC0769 Serial No PCE BC0771 thru Serial No PCE BC0785 and
Effectivity PW206C Engines which are before and include Serial No. PCE-BC0774. PW207C Engines which are before and include Serial No. PCE-BH0328. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE
SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
APLICAR, NUMERO DE SERIE DE LOSMOTOR. LH S/N PCE-BH-0141, RH S/NPCE-BH-0128.
798.- P&WC S.B. No. 28306 R2 CATEGORY 7 4-Feb-10 Once
799.- P&WC S.B. No. 28310 R1 CATEGORY 7 21-Apr-10 Once
800 P&W SB28314 CATEGORY 7 10 Nov 09 Once
TURBOSHAFT ENGINE DISK BALANCING ASSEMBLY, COMPRESSOR TURBINE - REPLACEMENT OF "ENGINE LH & RH"
Effectivity, PW206B2 Engines. PW206C Engines. PW207C Engines. PW207D Engines. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
APLICAR, NUMERO DE SERIE DE LOSMOTOR. LH S/N PCE-BH-0141, RH S/NPCE-BH-0128.
Effectivity: PW206C Engines which are before and include Serial No. PCE-BC0769, Serial No. PCE-BC0771 thru Serial No. PCE-BC0785 and Serial No. PCE-BC0787 thru PCE-BC0794. PW207C Engines which are before and include Serial No. PCE-BH0281, Serial No. PCE-BH0283 thru Serial No. Serial No. PCE-BH0305 and Serial No. PCE-BH0307 thru PCE-BH0376. CATEGORY 7 - You can do this service bulletin when
the supply of superseded parts is fully used. You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.
APLICAR, NUMERO DE SERIE DE LOSMOTOR. LH S/N PCE-BH-0141, RH S/NPCE-BH-0128.
TURBOSHAFT ENGINE REDUCTION GEARBOX HOUSING, REAR - Effectivity PW207C Engines which are before and include Serial No. PCE-BH0478. CATEGORY 5 - P&WC recommends to do this service
bulletin when the engine is disassembled and access is available to the necessary subassembly (i e module accessories components or build APLICAR NO HAY800.- P&W SB28314 CATEGORY 7 10-Nov-09 Once
801.- SAIB NE-10-28 RECOMMENDED 22-Apr-10 Once
802.- AD2010-09-04 39-16269 14-May-10 Once - May-10 - 14 DAYS - - 28-May-10 -
TURBOSHAFT ENGINE REDUCTION GEARBOX HOUSING, REAR REPLACEMENT/MODIFICATION OF LH & RH bulletin when the engine is disassembled and access is available to the necessary subassembly (i.e. module, accessories, components, or build
groups). Do all spare subassemblies. APLICAR.
TO PROVIDE THE FLIGHTCREW WITH PROCEDURES TO RECOVER FROM OR WORK AROUND THESE SOFTWARE ANOMALIES DURING FLIGHT.
VERIFICAR POR EQUIPOINSTALADO.
C OGARANTIA
The FAA reminds owners and operators of aircraft that loose equipment on the glare shield or in the cockpit can present a hazard particularly AGREGAR UNA COPIA AL
TURBINE ENGINE OPERATION IN VOLCANIC ASH AIRSPAEC. TO HIGHLIGHT RECENT ACTIONS AND EMPHASIZE THE NEED FOR OPERATOR AWARENESS. AGREGAR UNA COPIA AL MANUAL DE VUELO DE LA AERONAVE.
AGREGAR UNA COPIA ALMANUAL DE VUELO DE LAAERONAVE.
803.- SAIB CE-10-35 RECOMMENDED 24-May-10 OnceThe FAA reminds owners and operators of aircraft that loose equipment on the glare shield or in the cockpit can present a hazard, particularly for aircraft with a windshield heater system installed where electrical terminal strips may be exposed and subject to short circuit. AGREGAR
UNA COPIA AL MANUAL DE VUELO DE LA AERONAVE.
AGREGAR UNA COPIA ALMANUAL DE VUELO DE LAAERONAVE.
Loose Equipment in the Flight Compartment and on Glare Shields
Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.