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C:\DOCUME~1\e3user\LOCALS~1\Temp\e3temp_3412\.aptcache\ae2mssx3/tf2msuwaREASON
This sheet transmits Revision 1 to SB680-34-20, which: A. Changes
the serial effectivity.
B. Changes the title from EPIC Phase 5 Software Upgrade to EPIC
Phase 5.2 Software Upgrade.
C. Changes the EPIC Phase 5 to EPIC Phase 5.2.
D. Adds Honeywell Pilot's Guide Temporary Revision sheets to the
SB680-34-20-0 Kit.
E. Makes editorial changes throughout the document.
NOTE: This revision replaces the original issue of SB680-34-20 in
its entirety.
NOTE: Change bars are used in this publication to denote revised
material.
REVISION COMPLIANCE
MANDATORY COMPLIANCE. Airplanes 680-0291 thru -0323 and airplanes
that have previously complied with the original release of this
service bulletin must do Step 2 of this revision within 400 flight
hours or 1 year from the date of receipt, whichever occurs
first.
NOTE: For airplanes 680-0001 thru -0290 equipped with any EPIC
Phase software prior to 5.0, compliance with this service bulletin
remains recommended.
LOG OF REVISIONS
Original Issue June 25, 2010
Revision 1 March 15, 2012
Original Issue - June 25, 2010 SB680-34-20 Revision 1 - March 15,
2012 Page 1 of 1
Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706,
Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271,
Email:
[email protected]
COPYRIGHT © 2010
EFFECTIVITY
680 (Citation Sovereign) -0001 thru -0323
NOTE: The accomplishment of this service bulletin will have no
affect on RVSM operations.
NOTE: (For airplanes 680-0001 thru -0140) SB680-34-10 Network
Interface Module Improvement must have been complied with prior to
or in conjunction with SB680-34-20R1.
NOTE: Certain airplanes may need additional hardware modifications
that require advance notification before completing this bulletin.
Check the Accomplishment Instructions section to determine what
airplanes are affected.
NOTE: Cessna Aircraft Company approves only a Cessna representative
(with instructions from Cessna Aircraft Company for this software
upgrade) or a Honeywell representative to complete this software
upgrade. After completion of this upgrade by a Cessna
representative or Honeywell representative as specified above, the
maintenance technician must show accomplishment of this service
bulletin with documentation in the airplane logbook for
installation of this software upgrade.
REASON
DESCRIPTION
This service bulletin provides the parts and instructions necessary
to update the Honeywell Primus Epic software to Phase 5.2.
COMPLIANCE
RECOMMENDED. This service bulletin should be accomplished at a
scheduled maintenance period or Phase inspection.
A service bulletin published by Cessna Aircraft Company may be
recorded as “completed” in an aircraft log only when the following
requirements are satisfied:
1) The mechanic must complete all of the instructions in the
service bulletin, including the intent therein.
2) The mechanic must correctly use and install all applicable parts
supplied with the service bulletin kit. Only with written
authorization from Cessna Aircraft Company can substitute parts or
rebuilt parts be used to replace new parts.
3) The mechanic or airplane owner must use the technical data in
the service bulletin only as approved and published.
4) The mechanic or airplane owner must apply the information in the
service bulletin only to aircraft serial numbers identified in the
“Effectivity” section of the bulletin.
5) The mechanic or airplane owner must use maintenance practices
that are identified as acceptable standard practices in the
aviation industry and governmental regulations.
Original Issue - June 25, 2010 SB680-34-20 Revision 1 - March 15,
2012 Page 1 of 18
Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706,
Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271,
Email:
[email protected]
COPYRIGHT © 2010
Citation SERVICE BULLETIN SB680-34-20
No individual or corporate organization other than Cessna Aircraft
Company is authorized to make or apply any changes to a
Cessna-issued service bulletin, service letter, or flight manual
supplement without prior written consent from Cessna Aircraft
Company.
Cessna Aircraft Company is not responsible for the quality of
maintenance performed to comply with this document, unless the
maintenance is accomplished at a Cessna-owned Citation Service
Center.
APPROVAL
Cessna received FAA approval for the technical data in this
publication that changes the airplane type design.
This information is an amendment to the applicable maintenance
manual, and Cessna recommends that you complete it within the
scheduled time period.
FLIGHT CREW OPERATIONS
TOOLING
NAME USE
Laptop PC configured for Epic software loading To install the Epic
Phase 5.2 software
In addition to the above tooling, the following references the
source for the software installation:
• Flight Software CD - Honeywell Media, Part Number MM7031847-015.
• Tools CD - TM7035295-012, required to load EPIC software. • FMS
Navigation Database CD - Available by monthly subscription. •
Electronic Charts Database CD - Available by monthly subscription.
(If electronic charts are installed.) • Options CD - DM7038647-XXX
(-XXX will depend on the options that the airplane is configured
with). • TOLD CD - DM7037751-01003, delivered with airplane, or
delivered in SB680-34-20. • Previous version Flight Software CD -
Part number MM7031847-XXX, delivered with airplane, or
delivered
in the latest service bulletin incorporated. • Epic standard
database CD - 8940408-5, containing:
• 998-3822-505 (if CMF is installed and the service provider is
SATCOM Direct) • 6918234-3 ARES Config • 8941001-20 CMC LDI •
9988301-5 ARES View 1.4 • 60000696-001-06 FMS Aircraft Database •
69001249-501 (if CMF is installed and the service provider is GDC)
• 89220025 FDR DB (w/o FDAU) • 89220026 FDR DB (w/ FDAU) •
CitSovNone2.ecl Blank Checklist (if there is no operator developed
checklist) • DMU Loader (Cessna developed loader tool) •
XAA-C0150-0004P (if CMF is installed and service provider is ARINC
Direct)
WEIGHT AND BALANCE INFORMATION
PUBLICATIONS AFFECTED
Cessna Model 680 FAA Approved Airplane Flight Manual
Citation SERVICE BULLETIN SB680-34-20
ACCOMPLISHMENT INSTRUCTIONS
1. For airplanes -0001 thru -0290 that have not previously complied
with the original issue of this service bulletin, do Steps 3 thru
31.
2. For airplanes -0001 thru -0290 that have previously complied
with the original issue of this service bulletin and airplanes
-0291 thru -0323 that have EPIC PHASE 5.0, do the following:
A. Prepare the airplane for electrical power.
(1) Make sure that all switches are in the OFF/NORM position.
(2) Connect electrical power to the airplane.
(a) Connect the airplane batteries.
(b) Connect external electrical power.
(c) Make sure airplane is in the ground mode either with weight on
wheels or by using squat switch simulators.
(d) Make sure engine FADECs are installed.
(e) Make sure FADEC circuit Breakers HT102, HT103, HT202 &
HT203 are engaged.
NOTE: Epic will default to IN AIR mode if no input from the FADECs
is present. The software load will fail if the airplane is in air
mode.
(f) Turn power on.
B. Connect a laptop computer to the LAN port on the left aft area
of the pedestal.
C. Disable any wireless connection from the laptop. The upload of
the software will fail if a wireless connection is in use.
D. Make sure the laptop is configured with the tools CD
TM7035295-012.
E. Record the APM settings using the existing MM7031847-XXX
Software Definition for use later.
NOTE: The CD version must match the software version EPIC Phase 5.0
that is installed in the airplane.
(1) Put the flight software CD MM7031847-015 into the CD
drive.
(2) Start the APM settings tool on the laptop.
(3) Select the button with three dots that is to the right of the
"SETTING.DEF" file.
(4) In the folder list that appears, navigate through the CD drive
to the folder named "APM_DEFN" and open the folder.
(5) Select the "SETTINGS.DEF" file, and select "OPEN".
(6) After the folder window closes, leaving the APM tool window,
select "OPEN" again.
(7) Select "GET APM LIST".
NOTE: After a few moments, the drop down list to the left will fill
with NIC's to choose from. Some of the cockpit displays may become
unusable at this time.
(8) Select "LOAD from APM".
NOTE: After a few moments, a screen will appear where the airplane
options can be viewed. At the bottom of the window, buttons labeled
"NEXT PAGE" and "PREVIOUS PAGE" can be used to flip through the
available options.
SB680-34-20 Revision 1 - March 15, 2012 Page 3
SB680-34-20 Page 4 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
F. (For airplanes with electronic charts installed) Record the
Jeppesen Serial Number by selecting "CHART" and record the 16 digit
number in the SERIAL NUMBER field of the revision info
screen.
NOTE: The new load will erase the number and failure to do this
will disable charts until the number is re-entered.
G. Install the software that follows: • Epic operational software
MM7031847-015 using the FULL LOAD method. • Epic APM options
software that was determined in the MATERIAL INFORMATION
section
at the end of this bulletin.
H. If the airplane has CMF installed, and the Honeywell Global Data
Center (GDC) is the service provider, then install the CMF AMI
69001249-501 from the Epic Standard Database CD.
I. If the airplane has CMF installed and ARINC Direct is the
service provider, then install the new CMF AMI XAA-C0150-0004P from
the Epic Standard Database CD.
NOTE: The service provider can be determined by looking at the
information that was recorded in Step 2E.
For GDC and SATCOM Direct:
2 character IATA ID = GS
3 character ICAO ID = GDC
For ARINC:
2 character IATA ID = XA
3 character ICAO ID = XAA
J. If the airplane has CMF installed and SATCOM Direct is the
service provider, then install the CMF AMI 998-3822-505 from the
Epic Standard Database CD.
NOTE: The service provider can be determined by looking at the
information that was recorded in Step 2E.
For GDC and SATCOM Direct:
2 character IATA ID = GS
3 character ICAO ID = GDC
For ARINC:
K. If TOLD is installed, then install DM7037751-01003 TOLD
software.
L. Install 8941001-20 CMC LDI from the 8940408-5 Epic Standard
Database CD.
M. Install Electronic checklist.
NOTE: If the customer has a vendor supplied checklist, the vendor
supplied checklist will need to be updated to be compatible with
Phase 5. The checklist built for an airplane before Phase 5 will
not work on a Phase 5 airplane. If there is no customer checklist,
load CitSovNone2.ecl from the Cessna Epic standard database
CD.
N. Install the SVRGN-094000 FMS Aircraft Database from the
8940408-5 Epic Standard Database CD.
O. Check the database files that follow to make sure they are
unchanged.
NOTE: The databases listed below are not changed but they may need
to be reloaded or updated. • Charts Data, EGPWM envelope database,
EGPWM Terrain databse, NAV database
which are available on the current navigational database CD.
P. Update the settings you recorded in Step 2E.
(1) Put the flight software CD MM7031847-015 into the CD
drive.
Citation SERVICE BULLETIN SB680-34-20
(2) Start the APM settings tool on the laptop.
(3) Select the button with three dots that is to the right of the
"SETTING.DEF" file.
(4) In the folder list that appears, navigate through the CD drive
to the folder named "APM_DEFN" and open the folder.
(5) Select the "SETTINGS.DEF" file, and click on "OPEN"
(6) After the folder window closes, leaving the APM tool window,
select "OPEN" again.
(7) Select "LOAD FROM DEFINITION FILE".
(8) Update the APM settings you recorded in Step 2E.
NOTE: There will be new settings not recorded from the old
load.
(9) (For EASA registered airplanes only) Set FD Command Bar
Type.
NOTE: EASA certification requires the Command Bar Type to always
display either Cross Pointer or Single Cue. This may be determined
by pilot preference.
(a) For Single Cue then select “Single Cue on both PFDs” from the
drop down menu.
(b) For Cross Pointer then select “Cross Pointer on both PFDs” from
the drop down menu.
NOTE: Do not select “Crew Controlled-Independent” or “Crew
Controlled-Synchronized” on EASA registered airplanes.
(10) The settings listed below will need to be entered: • APU
Engine Control Unit - Select appropriate ECU part number. • Battery
Type - NiCAD. • CMF Network Type - "AOA" if 7026201-803 CMF radio
is installed, "POA" if 7026201-804
CMF radio is installed. • FDR Installed - "Installed" if FDR is
installed, "Not Installed" if not. • A/C Performance DBS Config. ID
- 94000. • GPS Sensor Type - CMC_C129. • RAAS APP Runway In Air -
Enable. • RAAS APP Short Runway Length - 3000. • RAAS Distance
Units - Feet. • RAAS Dist Remain Land Rollout - Enable. • RAAS Dist
Remain RTO - Enable. • RAAS Dist Remain Advisory Vol -Default
Volume (At normal EGPWS Volume). • RAAS Gnd Short Runway Length -
3300. • RAAS Antenna Location - 14. • RAAS in Air Advisory Vol -
Default Volume (6db below normal EGPWS Volume). • RAAS Inhibit Type
- Independent Cockpit RAAS Inhibit Selection. • RAAS Initial Hold
Time - 90 seconds. • RAAS On Ground Advisory Vol - Default Volume
(6db below normale EGPWS Volume). • RAAS On Taxiway Advisory Vol -
Default Volume (At normal EGPWS Volume). • RAAS Repeat Hold Time -
120 seconds. • RAAS Runway End - Enable. • RAAS Taxiway Takeoff -
Enable. • RAAS Voice Gender - Female Voice. • TOLD Runway Factor
For Dry - 1.67. • TOLD Runway Factor For Wet - 1.92. • VDR Transfer
Tone - Disable
(11) Use the "NEXT PAGE" button to get to the next page and enter
the appropriate settings on each page.
SB680-34-20 Revision 1 - March 15, 2012 Page 5
SB680-34-20 Page 6 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
(12) Select "CREATE AND LOAD BINARY FILE" on the last page.
(a) A window will appear with a folder list. It is asking where to
save the file. Select a folder that has read-write access
permission. Normally this opens to the temporary folder which is
acceptable to use. Select "OPEN". If the box appears with the
question "FILE EXISTS, DO YOU WISH TO OVERWRITE", select
"YES".
(13) A window will show "ENTER DR FILE PART NUMBER". Leave it blank
and select "OK".
(14) After a few moments, a window will appear with an indication
of success or failure.
(a) If success is shown for all four APMs, select "OK", then
continue with Step 2P.
(b) If failure is shown for any APM continue to the next
step.
(15) Make a note of which APM's were successful.
(16) Select "OK".
(17) Close APM tool windows.
(18) Cycle electrical power off to the airplane, wait 30 seconds,
then cycle electrical power back on.
(19) Go to Step N.
Q. Cycle the airplane power.
CAUTION: Before turning the airplane power off, wait 3 minutes
after the last software load completes. Software data could be
corrupted or erased if this is not done.
(1) Turn the airplane power off.
NOTE: It is not necessary to disconnect external power.
(2) Wait a minimum of 3 minutes.
(3) Turn the airplane power on.
R. Do a check of the system software load.
(1) Make sure the airplane is in ground mode.
(2) Turn on all avionic systems and allow time for
initialization.
(3) Make sure the software version is correct.
(a) Use the copilot's Cursor Control Display (CCD), select the MAP
pull-down menu on DU3.
Citation SERVICE BULLETIN SB680-34-20
(b) Select SCMS and examine the SCMS pages to make sure the
software and database identifiers are correct.
1 Page 1: • Top level system part number EB7031847-00114. •
Configuration part number - TT7038647-XXX (determined by
Options
Configurator).
2 Page 2: • FMS1 A/C PERF 60000696-001-06. • FMS2 A/C PERF
60000696-001-06.
3 Page 4: • EGPWM Terrain - 996-0145-556 or later terrain database.
• EGPWM Envelope Modulation - 996-0114-518 or later envelope
database.
4 Page 5: • ECL 1 Checklist - CitSovNone2ecl (or file which was
created by the operator). • CMC 1 LDI - 8941001-20. • CMF1
AMI-69001249-501 (if CMF installed and GDC is the service
provider). • CMF1 AMI-998-3822-505 (if CMF installed and SATCOM
Direct is the service
provider). • CMF1 AMI XAA-C0150-0004P (if CMF installed and ARINC
Direct is the
service provider). • TOLD 1 Data C680-01-003-08MAR2007 (if TOLD
installed). • TOLD 2 Data C680-01-003-08MAR2007 (if TOLD
installed).
(c) Press CONFIRM on the SCMS screen after you make sure of each
identifier above.
(4) Make sure that the EICAS message "CONFIGURATION MISMATCH” is
not displayed.
NOTE: If the “CONFIGURATION MISMATCH" message is present, the
software load and/or hardware configuration is not correct. This
must be corrected before you continue with the instructions.
(5) Make sure that there is not a scratchpad message on either of
the MCDU’s indicating an invalid or expired NAV database.
NOTE: If there is a scratch pad message, the NAV database must be
loaded again.
(6) Review each display reasonable data and any EICAS messages that
are shown.
(a) The attitude is level.
(b) The heading corresponds to aircraft heading.
(c) The airspeed is 30 knots.
NOTE: The display parks at 30 knots.
(d) The altitude corresponds to the field elevation.
(7) Review EICAS for reasonable data.
(a) All messages are understood and accounted for.
(b) Make sure that there are no amber dashes on EICAS data.
(8) (For airplanes that have charts.) Make sure that the charts can
be selected for display using the CCD on the MFD.
(9) Do a test of the NAV radios.
(a) Tune NAV radios to a nearby NAV station using MCDU or
CCD.
(b) Press left PUSH DCT button on guidance controller.
(c) Make sure that the green NAV needle on pilots PFD points to the
NAV station.
SB680-34-20 Revision 1 - March 15, 2012 Page 7
SB680-34-20 Page 8 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
(d) Repeat for NAV 2, right PUSH DCT button and copilots PFD.
(10) Do a test of the COM radios.
(a) Tune the radios to nearby ATIS frequency.
(b) Adjust audio panel so that COM 1 audio is heard over
speakers.
(c) Make sure that the ATIS signal can be heard.
(d) Repeat for COM 2.
(11) (For Airplanes -0260 thru -0323.) Update the AReS Diagnostic
Recording Unit.
(a) Install 9988301 AReS View PC software located in the AReS
folder on the Epic Standard Database CD.
1 Open “AV_Install.zip” file. (Version 1.3 or later.)
2 Select “setup.exe”.
NOTE: For installation instructions, reference Chapter 6 of the
AReS View User’s Guide (rev D or later). A copy of this guide can
be found in the AReS folder on the Epic Standard Database CD titled
“AReSViewUsersGuide.pdf”.
(12) Update the AReS unit with the “680-003.cfg” (or later)
Configuration File located in the AReS folder on the Epic Standard
Database CD.
NOTE: For configuration instructions, reference Chapter 5 of the
AReS View User’s Guide (revision D or later).
NOTE: Copies of both the latest 680 AReS Configuration File and the
AReS View User’s Guide can also be downloaded from the 680 page at
CessnaSupport.com.
S. Update the Cessna Model 680 FAA approved Flight Manual
(68FM).
NOTE: Look at the configuration codes listed in the applicable
supplement and/or in Section 1 of the FAA Approved Airplane Flight
Manual to make sure all changed crew procedures or limitations are
complied with.
(1) Remove TC-R10-04, TC-R10-05, TC-R10-07 and TC-R10-08 from the
680 FAA Approved Airplane Flight Manual (68FM).
NOTE: TCs -04 and -05 state to remove them when SB680-34-31 is
installed. This was previously identified as the service bulletin
that would install the EPIC Phase 5.2 Software.
(2) Update the Cessna Model 680 FAA approved Flight Manual with
Revision 10 or later.
(a) Insert 68FM TC-R10-09 and TC-R10-10 into the 680 FAA Approved
Airplane Flight Manual (68FM).
(3) Insert the yellow FMS Pilot's Guide Temporary Revision No. 1
sheets provided with the service bulletin kit into Honeywell
Pilot's Guide for the Flight Management System (FMS) for the Cessna
Citation Sovereign Software Version NZ7.1.2. (part number
A28-1146-183 Revision 4 or later).
T. Go to step 28.
3. Prepare the airplane for maintenance.
A. Make sure that all switches are in the OFF/NORM position.
B. Disconnect electrical power from the airplane.
(1) Disconnect the airplane batteries.
(2) Disconnect external electrical power.
Citation SERVICE BULLETIN SB680-34-20
C. Attach maintenance warning tags to the batteries and external
power receptacle that have "DO NOT CONNECT ELECTRICAL POWER -
MAINTENANCE IN PROGRESS" on them.
4. (For airplanes 680-0115 thru -0213 that have electronic charts
installed and have not complied with SB680-34-23) Install the
7036410-1901 Advanced File Graphics Server (AFGS II). (Refer to the
Cessna Model 680 Maintenance Manual, Chapter 34, Modular Avionics
Unit - Maintenance Practices.)
A. Remove the 7026545-1903 Advanced File Graphics Server (AFGS I)
module from MAU 1, slots 2 and 3.
B. Install the AFGS II module in MAU 1 slots 2 (PN917) and 3
(PN919).
C. Return the 7026545-1903 AFGS I module to Citation Parts
Distribution.
5. (For airplanes 680-0001 thru -0213 with CMF that have not
complied with SB680-34-23) Make sure the mod level of the
7026201-804 CMF radio is MOD D or later.
A. If the CMF radio has the required mod level, go to Step 6.
B. If the CMF radio does not have the required mod level, return
the radio to Cessna for an upgrade.
NOTE: Operators: The existing 7026201-804 CMF Radio may be
modified. Cessna Service Parts & Programs Avionics team to
schedule modification at 1.316.517.1651 or telefax 1.316.206-5044
or email
[email protected]. This will require advance
notification. The Cessna Service Parts & Programs Avionics team
will schedule the units and arrange for their return. Please allow
five to seven days for modification. This service bulletin may not
be signed off as completed unless the units are scheduled through
Citation Parts Distribution.
(1) Remove the CMF radio module. (Refer to the Model 680
Maintenance Manual, Chapter 23, Honeywell Communications Management
Function (CMF) Radio Module - Maintenance Practices.)
(2) Install the upgraded CMF radio module. (Refer to the Model 680
Maintenance Manual, Chapter 23, Honeywell Communications Management
Function (CMF) Radio Module - Maintenance Practices.)
6. Get access to the HF power amplifiers or provisions if
installed. (Refer to the Cessna Model 680 Maintenance Manual,
Chapter 23, Honeywell KHF-1050 Hf Communication System -
Maintenance Practices.)
A. Remove access panel 312BTC. (Refer to the Cessna Model 680
Maintenance Manual, Chapter 6, Access Plates And Panels
Identification - Description And Operation.)
NOTE: The electrical connectors PT529 and PT530 are located on the
forward side of the power amplifiers.
B. Do the HF1 wiring changes. If HF 1 is not installed, go to Step
7.
(1) Install two TMS3/16-1-1.50 Sleeves marked 23PT529-27PT925 on
each end of the wire marked 11PT529-27PT925.
(2) Install two TMS3/16-1-1.50 Sleeves marked 11PT529-BTSG11 on
each end of the wire marked 23PT529-BTSG11.
(3) Update the customer's avionics wirebook with a copy of this
page.
(4) Changes are shown below.
SB680-34-20 Revision 1 - March 15, 2012 Page 9
SB680-34-20 Page 10 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
C. Do the HF2 wiring changes. If HF2 is not installed, go to Step
7.
(1) Install two TMS3/16-1-1.50 Sleeves marked 23PT530-27PT926 on
each end of the wire marked 11PT530-27PT926.
(2) Install two TMS3/16-1-1.50 Sleeves marked 11PT530-BTSG21 on
each end of the wire marked 23PT530-BTSG21.
(3) Update the customer's avionics wirebook with a copy of this
page.
(4) Changes are shown below.
Citation SERVICE BULLETIN SB680-34-20
7. (For airplanes that only need to install the EPIC Phase 5.2
software.) Prepare the airplane for electrical power.
A. Make sure that all switches are in the OFF/NORM position.
B. Connect electrical power to the airplane.
(1) Connect the airplane batteries.
(2) Connect external electrical power.
(3) Make sure airplane is in the ground mode either with weight on
wheels or by using squat switch simulators.
(4) Make sure engine FADECs are installed.
(5) Make sure FADEC circuit Breakers HT102, HT103, HT202 &
HT203 are engaged
NOTE: Epic will default to IN AIR mode if no input from the FADECs
is present. The software load will fail if the airplane is in air
mode.
(6) Turn power on.
8. Connect a laptop computer to the LAN port on the left aft area
of the pedestal.
9. Disable any wireless connection from the laptop. The upload of
the software will fail if a wireless connection is in use.
10. Make sure the laptop is configured with the tools CD
TM7035295-012.
11. Record the APM settings using the existing MM7031847-XXX
Software Definition for use later.
NOTE: The CD version must match the software version (Epic Phase 3,
4, 4.1, 4.2 or 5.0) that is installed in the airplane.
A. A. Put the flight software CD MM7031847-015 into the CD
drive.
B. Start the APM settings tool on the laptop.
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Citation SERVICE BULLETIN SB680-34-20
C. Select the button with three dots that is to the right of the
"SETTING.DEF" file.
D. In the folder list that appears, navigate through the CD drive
to the folder named "APM_DEFN" and open the folder.
E. Select the "SETTINGS.DEF" file, and select "OPEN".
F. After the folder window closes, leaving the APM tool window,
select "OPEN" again.
G. Select "GET APM LIST".
NOTE: After a few moments, the drop down list to the left will fill
with NIC's to choose from. Some of the cockpit displays may become
unusable at this time.
H. Select "LOAD from APM".
NOTE: After a few moments, a screen will appear where the airplane
options can be viewed. At the bottom of the window, buttons labeled
"NEXT PAGE" and "PREVIOUS PAGE" can be used to flip through the
available options.
12. (For airplanes with electronic charts installed) Record the
Jeppesen Serial Number by selecting "CHART" and record the 16 digit
number in the SERIAL NUMBER field of the revision info
screen.
NOTE: The new load will erase the number and failure to do this
will disable charts until the number is re-entered.
13. Install the software that follows: • Epic operational software
MM7031847-015 using the FULL LOAD method. • Epic APM options
software that was determined in the MATERIAL INFORMATION section at
the
end of this bulletin.
14. If the airplane has CMF installed, and the Honeywell Global
Data Center (GDC) is the service provider, then install the CMF AMI
69001249-501 from the Epic Standard Database CD.
15. If the airplane has CMF installed and ARINC Direct is the
service provider, then install the new CMF AMI XAA-C0150-0004P from
the Epic Standard Database CD.
NOTE: The service provider can be determined by looking at the
information that was recorded in Step 11. For GDC: 2 character IATA
ID = GS 3 character ICAO ID = GDC For ARINC: 2 character IATA ID =
XA 3 character ICAO ID = XAA
16. If the airplane has CMF installed and SATCOM Direct is the
service provider, then install the CMF AMI 998-3822-505 from the
Epic Standard Database CD.
NOTE: The service provider can be determined by looking at the
information that was recorded in Step 2E. For GDC and SATCOM
Direct: 2 character IATA ID = GS 3 character ICAO ID = GDC For
ARINC: 2 character IATA ID = XA 3 character ICAO ID = XAA
17. If TOLD is installed, then install DM7037751-01003 TOLD
software.
18. Install 8941001-20 CMC LDI from the 8940408-5 Epic Standard
Database CD.
19. Install Electronic checklist.
NOTE: If the customer has a vendor supplied checklist, the vendor
supplied checklist will need to be updated to be compatible with
Phase 5. The checklist built for an airplane before Phase 5 will
not work on a Phase 5 airplane. If there is no customer checklist,
load CitSovNone2.ecl from the Cessna Epic standard database
CD.
Citation SERVICE BULLETIN SB680-34-20
20. Install the SVRGN-094000 FMS Aircraft Database from the
8940408-5 Epic Standard Database CD.
21. Check the database files that follow to make sure they are
unchanged.
NOTE: The databases listed below are not changed but they may need
to be reloaded or updated. • Charts Data, EGPWM envelope database,
EGPWM Terrain databse, NAV database which are
available on the current navigational database CD.
22. Update the settings you recorded in Step 11.
A. Put the flight software CD MM7031847-015 into the CD
drive.
B. Start the APM settings tool on the laptop.
C. Select the button with three dots that is to the right of the
"SETTING.DEF" file.
D. In the folder list that appears, navigate through the CD drive
to the folder named "APM_DEFN" and open the folder.
E. Select the "SETTINGS.DEF" file, and click on "OPEN"
F. After the folder window closes, leaving the APM tool window,
select "OPEN" again.
G. Select "LOAD FROM DEFINITION FILE".
H. Update the APM settings you recorded in Step 11.
NOTE: There will be new settings not recorded from the old
load.
I. (For EASA registered airplanes only) Set FD Command Bar
Type.
NOTE: EASA certification requires the Command Bar Type to always
display either Cross Pointer or Single Cue. This may be determined
by pilot preference.
(1) For Single Cue then select “Single Cue on both PFDs” from the
drop down menu.
(2) For Cross Pointer then select “Cross Pointer on both PFDs” from
the drop down menu.
NOTE: Do not select “Crew Controlled-Independent” or “Crew
Controlled-Synchronized” on EASA registered airplanes.
J. The settings listed below will need to be entered: • APU Engine
Control Unit - Select appropriate ECU part number. • Battery Type -
NiCAD. • CMF Network Type - "AOA" if 7026201-803 CMF radio is
installed, "POA" if 7026201-804
CMF radio is installed. • FDR Installed - "Installed" if FDR is
installed, "Not Installed" if not. • A/C Performance DBS Config. ID
- 94000. • GPS Sensor Type - CMC_C129. • RAAS APP Runway In Air -
Enable. • RAAS APP Short Runway Length - 3000. • RAAS Distance
Units - Feet. • RAAS Dist Remain Land Rollout - Enable. • RAAS Dist
Remain RTO - Enable. • RAAS Dist Remain Advisory Vol -Default
Volume (At normal EGPWS Volume). • RAAS Gnd Short Runway Length -
3300. • RAAS Antenna Location - 14. • RAAS in Air Advisory Vol -
Default Volume (6db below normal EGPWS Volume). • RAAS Inhibit Type
- Independent Cockpit RAAS Inhibit Selection. • RAAS Initial Hold
Time - 90 seconds. • RAAS On Ground Advisory Vol - Default Volume
(6db below normale EGPWS Volume). • RAAS On Taxiway Advisory Vol -
Default Volume (At normal EGPWS Volume). • RAAS Repeat Hold Time -
120 seconds. • RAAS Runway End - Enable. • RAAS Taxiway Takeoff -
Enable.
SB680-34-20 Revision 1 - March 15, 2012 Page 13
SB680-34-20 Page 14 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
• RAAS Voice Gender - Female Voice. • TOLD Runway Factor For Dry -
1.67. • TOLD Runway Factor For Wet - 1.92. • VDR Transfer Tone -
Disable
K. Use the "NEXT PAGE" button to get to the next page and enter the
appropriate settings on each page.
L. Select "CREATE AND LOAD BINARY FILE" on the last page.
(1) A window will appear with a folder list. It is asking where to
save the file. Select a folder that has read-write access
permission. Normally this opens to the temporary folder which is
acceptable to use. Select "OPEN". If the box appears with the
question "FILE EXISTS, DO YOU WISH TO OVERWRITE", select
"YES".
M. A window will show "ENTER DR FILE PART NUMBER". Leave it blank
and select "OK".
N. After a few moments, a window will appear with an indication of
success or failure.
(1) If success is shown for all four APMs, select "OK", then
continue with Step 22.
(2) If failure is shown for any APM continue to the next
step.
O. Make a note of which APM's were successful.
P. Select "OK".
Q. Close APM tool windows.
R. Cycle electrical power off to the airplane, wait 30 seconds,
then cycle electrical power back on.
S. Go to Step 21.
23. Cycle the airplane power.
CAUTION: Before turning the airplane power off, wait 3 minutes
after the last software load completes. Software data could be
corrupted or erased if this is not done.
A. Turn the airplane power off.
NOTE: It is not necessary to disconnect external power.
B. Wait a minimum of 3 minutes.
C. Turn the airplane power on.
24. Do a check of the system software load.
A. Make sure the airplane is in ground mode.
B. Turn on all avionic systems and allow time for
initialization.
C. Make sure the software version is correct.
(1) Use the copilot's Cursor Control Display (CCD), select the MAP
pull-down menu on DU3.
(2) Select SCMS and examine the SCMS pages to make sure the
software and database identifiers are correct.
(a) Page 1: • Top level system part number EB7031847-00114. •
Configuration part number - TT7038647-XXX (determined by Options
Configurator).
(b) Page 2: • FMS1 A/C PERF 60000696-001-06. • FMS2 A/C PERF
60000696-001-06.
Citation SERVICE BULLETIN SB680-34-20
(c) Page 4: • EGPWM Terrain - 996-0145-556 or later terrain
database. • EGPWM Envelope Modulation - 996-0114-518 or later
envelope database.
(d) Page 5: • ECL 1 Checklist - CitSovNone2ecl (or file which was
created by the operator). • CMC 1 LDI - 8941001-20. • CMF1
AMI-69001249-501 (if CMF installed and GDC is the service
provider). • CMF1 AMI-998-3822-505 (if CMF installed and SATCOM
Direct is the service
provider). • CMF1 AMI XAA-C0150-0004P (if CMF installed and ARINC
Direct is the service
provider). • TOLD 1 Data C680-01-003-08MAR2007 (if TOLD installed).
• TOLD 2 Data C680-01-003-08MAR2007 (if TOLD installed).
(3) Press CONFIRM on the SCMS screen after you make sure of each
identifier above.
D. Make sure that the EICAS message "CONFIGURATION MISMATCH” is not
displayed.
NOTE: If the “CONFIGURATION MISMATCH" message is present, the
software load and/or hardware configuration is not correct. This
must be corrected before you continue with the instructions.
E. Make sure that there is not a scratchpad message on either of
the MCDU’s indicating an invalid or expired NAV database.
NOTE: If there is a scratch pad message, the NAV database must be
loaded again.
F. Review each display reasonable data and any EICAS messages that
are shown.
(1) The attitude is level.
(2) The heading corresponds to aircraft heading.
(3) The airspeed is 30 knots.
NOTE: The display parks at 30 knots.
(4) The altitude corresponds to the field elevation.
G. Review EICAS for reasonable data.
(1) All messages are understood and accounted for.
(2) Make sure that there are no amber dashes on EICAS data.
H. (For airplanes that have charts.) Make sure that the charts can
be selected for display using the CCD on the MFD.
I. Do a test of the NAV radios.
(1) Tune NAV radios to a nearby NAV station using MCDU or
CCD.
(2) Press left PUSH DCT button on guidance controller.
(3) Make sure that the green NAV needle on pilots PFD points to the
NAV station.
(4) Repeat for NAV 2, right PUSH DCT button and copilots PFD.
J. Do a test of the COM radios.
(1) Tune the radios to nearby ATIS frequency.
(2) Adjust audio panel so that COM 1 audio is heard over
speakers.
(3) Make sure that the ATIS signal can be heard.
(4) Repeat for COM 2.
SB680-34-20 Revision 1 - March 15, 2012 Page 15
SB680-34-20 Page 16 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
25. (For Airplanes -0260 thru -0323.) Update the AReS Diagnostic
Recording Unit.
A. Install 9988301 AReS View PC software located in the AReS folder
on the Epic Standard Database CD.
(1) Open “AV_Install.zip” file. (Version 1.3 or later.)
(2) Select “setup.exe”.
NOTE: For installation instructions, reference Chapter 6 of the
AReS View User’s Guide (rev D or later). A copy of this guide can
be found in the AReS folder on the Epic Standard Database CD titled
“AReSViewUsersGuide.pdf”.
B. Update the AReS unit with the “680-003.cfg” (or later)
Configuration File located in the AReS folder on the Epic Standard
Database CD.
NOTE: For configuration instructions, reference Chapter 5 of the
AReS View User’s Guide (revision D or later).
NOTE: Copies of both the latest 680 AReS Configuration File and the
AReS View User’s Guide can also be downloaded from the 680 page at
CessnaSupport.com.
26. Update the Cessna Model 680 FAA approved Flight Manual
(68FM).
NOTE: Look at the configuration codes listed in the applicable
supplement and/or in Section 1 of the FAA Approved Airplane Flight
Manual to make sure all changed crew procedures or limitations are
complied with.
A. Update the Cessna Model 680 FAA approved Flight Manual with
Revision 10 or later.
(1) Insert 68FM TC-R10-09 and TC-R10-10 into the 680 FAA Approved
Airplane Flight Manual (68FM).
27. Contact Honeywell International Inc.
NOTE: This step is only required for operators upgrading from Phase
4.2 to Phase 5.2.
NOTE: The yellow sheets provided in this kit are also included in
the Honeywell (FMS) Pilots Guide described below.
• Contact Honeywell International Inc. at phone number 800-601-3099
(US Customers) or 601-365-3099 (International Customers) to request
a copy of the Honeywell Pilot's Guide for the Primus Epic
Integrated Avionics System for the Cessna Citation Sovereign (Phase
V). (part number A28-1146-168 Revision 3 or later).
• Contact Honeywell International Inc. at phone number 800-601-3099
(US Customers) or 601-365-3099 (International Customers) to request
a copy of the Honeywell Pilot's Guide for the Flight Management
System (FMS) for the Cessna Citation Sovereign Software Version
NZ7.1.2. (part number A28-1146-183 Revision 4 or later).
28. Contact Honeywell FMS data base services to request access to
the unrestricted database.
A. Operators may request the unrestricted database after the
upgrade to Epic Phase 5.2 has been completed (part number
EB7031847-00114 Rev A or later).
NOTE: Fleet operators will not be allowed access to the
unrestricted database until all airplanes have been updated to Epic
Phase 5.2.
• For airplanes that have charts and maps, call INDS Data Base
Services at 888-309-7555 (US Customers) or 303-328-6948
(International Customers).
• For airplanes that do not have charts and maps, call FMS Data
Base Services at 602-436-6738 (US Customers).
29. Remove power from the airplane.
A. Make sure all switches are in the OFF/NORM position.
B. Disconnect external electrical power.
Citation SERVICE BULLETIN SB680-34-20
30. Make sure that the Flight Crew Operations Summary included with
this service bulletin is given to the crew to inform them of the
operational changes resulting from incorporation of this service
bulletin.
31. Record that you have completed this service bulletin.
A. Complete a Maintenance Transaction Report.
B. Put a copy of the completed Maintenance Transaction Report in
the airplane logbook.
C. Send a copy of the completed Maintenance Transaction Report to:
CESCOM C/O Camp Systems International 8200 E. 34th Street N.
Building 1600 Suite 1607 Wichita, KS 67226.
MATERIAL INFORMATION
NEW P/N QUAN- TITY
SB680-34-20-0 1 Kit, consisting of the following parts:
A28-1146-183-R004 TR1
1 Honeywell FMS Pilot's Guide A28-1146-183 Temp Revision No.
1
Insert yellow pages into the Honeywell Pilot's Guide
DM7037751-01003 1 Told Database CD
MM7031847-015 1 Epic Flight Software
TM7035295-012 1 Epic Tools Software CD
8940408-5 1 Epic Standard Database
SB680-34-20 1 Instructions
For airplanes that need to do the wiring modification in Step 6,
order the kit listed below.
NEW P/N QUAN- TITY
SB680-34-20-1 1 Kit, consisting of the following parts:
TMSSCE3/16-2.0-9 2 Sleeve marked 23PT529-27PT925
None
None
None
None
SB680-34-20 1 Instructions
For airplanes that have not complied with SB680-34-23, the part
listed below will be required to complete this service bulletin In
addition to the above kit.
SB680-34-20 Revision 1 - March 15, 2012 Page 17
SB680-34-20 Page 18 Revision 1 - March 15, 2012
Citation SERVICE BULLETIN SB680-34-20
NEW P/N QUAN- TITY
7036410-1901 If Required
1 AFGS II None
For airplanes that have do not have the current mod level D, the
part listed below will be required to complete this service
bulletin In addition to the above kit.
NEW P/N QUAN- TITY
7026201-804 If Required
1 CMF Radio 7026201-804 Return to Cessna for upgrade
NOTE: Operators: The existing 7026201-804 CMF Radio may be
modified. Cessna Service Parts & Programs Avionics team to
schedule modification at 1.316.517.1651 or telefax 1.316.206-5044
or email
[email protected]. This will require advance
notification. The Cessna Service Parts & Programs Avionics team
will schedule the units and arrange for their return. Please allow
five to seven days for modification. This service bulletin may not
be signed off as completed unless the units are scheduled through
Citation Parts Distribution.
In addition to the Service Bulletin Kit, you must order the
appropriate Options CD for your airplane. To determine the correct
part number do one of the following.
1. Use the Cessna online Options CD Configuration Utility. You must
have access to the “Customer Access” section of CessnaSupport.com
to use the utility. • Go to www.cessnasupport.com. • Click on
“Customer Access”. • Log in using your Login ID and Password. •
Under My Models select “Citation 680”. • Under Maintenance
Information select “Epic Options Configuration Utility”.
2. If you do not have access to CessnaSupport.com, contact Cessna
Service Parts & Programs or Team Sovereign directly to obtain
correct Phase 5.2 Options CD part number to order.
• Cessna Service Parts & Programs
Phone 1-800-835-4000 or 1-316-517-6273
FLIGHT CREW OPERATIONS SUMMARY
This summary provides additional information for the flight crew
regarding operational changes as a result of accomplishment of this
service bulletin. Please remove this summary from the service
bulletin and give it to the flight crew. This summary does not
supersede any information in the FAA Approved Airplane Flight
Manual. The changes that follow are for information only. The
following list applies for those airplanes that update to EPIC
Phase 5.0 and are also part of the EPIC Phase 5.2 baseline. • Adds
arrow head to the turn direction indicator on the MFD MAP. •
Eliminated a possible cause for AP FAIL on initial engagement. •
Changes minimums aural to prevent multiple callouts if the airplane
encounters turbulence. • Adds capability to prepare flight plans
off airplane, save on CD or PCMCIA card, then load into FMS
using
the DMU. Flight plans can also be prepared using GDC, saved, then
loaded with DMU. • Adds APU ON EICAS message. • Speeds up power up
of DU hardware 2 from 20 seconds to 10 seconds. • Changes flight
director overspeed operation to not nose down the airplane in
certain scenarios. • Adds debounce to SPEED BRAKES EICAS message to
prevent nuisance at landing. • Fixes issue where TOLD Vspeeds were
lost after avionics power on. • Eliminates nuisance MONITOR WARNING
FAIL message at power on. • Adds TX indication for COM radios to
MFD and EICAS. • Adds MCDU scratchpad message to indicate when
uplink weather is available for display on MFD. • Allows manual
entry of weights up to 30,300 lbs in TOLD. • Adds approach Vspeed
preview to airspeed tape. • Adds setting for TOLD landing factors,
operators can now set the default factor in the APM settings. •
Adds VHF frequency change blip to APM settings. The radio will beep
when the frequency is changed, if
the APM setting is set. This is in the operator controlled area of
the APM. • Changes CCD timeout locations to prevent inadvertent COM
frequency changes. • Changes sorting of charts in picklist to put
airport briefing pages in correct order. • Changes FMS to allow
holds to be placed at the FAF. • Adds XPDR STBY EICAS message to
let you know if the transponder is off. • Adds TCAS display to the
PFD. This is selectable on the MCDU menu page. • Lowers volume of
altitude alert, phone call aural, SELCAL aural. • RNP SAAAR/AR 0.3
with RF Legs (curved path), missed approach RNP 1.0. • Adds
automatic LOC preview. FMS will automatically setup a preview
capture when an ILS approach
is loaded. • Fixes most FMS VNAV splits. • Numerous FMS
improvements. • Enables Uplink WX on airplanes that are equipped
with Uplink WX. Added support for optional systems. The following
are not included as part of this service bulletin, but the software
has been updated to work with these options. There are plans to
make some of these available to the field, depending on operator
interest. Please contact Team Sovereign if you are interested in
purchasing any of these options:
• WAAS/LPV approaches - improves GPS accuracy, and allows LPV
approaches with AP coupling. • RAAS - Runway Awareness and Advisory
System. • IRS - Allow RNP SAAAR approaches with a missed approach
< 1.0 (to a minimum of 0.3).
Known Issues carried over from Phase 5.0: • The trim clacker aural
is different than before. • FMS guidance is not displayed on the
standby HSI in emergency power. • Any customer supplied checklist
will need to be rebuilt to be compatible with Phase 5. • HF test on
HF 2 causes the HF2 to lock up.
Citation ATTACHMENT SB680-34-20
• Nuisance OAT/ISA LIMIT EXCEEDED with avionics off. • FMS APU fuel
flow and fuel used indications always read 0.
NOTE: This only applies to aircraft with 9914657-3 APU ECU’s
installed.
• The Change over feature does not work properly.
NOTE: When Change Over is selected while flying a mach target
value, the airspeed target may remain in mach mode and possibly
change to a different mach target value. Operation depends on the
altitude when FLC is initially engaged. If the altitude is above
28000 feet in a climb, or above 29800 feet in a descent, when FLC
is initially engaged, the Change Over button will have incorrect
operation.
The following list applies to the Phase 5.2 changes. • Corrects a
pitch down condition occurring when capturing the ILS GS. • Fixes
auto-preview not properly updating the course when the approach
procedure is changed. • Prevents nuisance MAU OVERTEMP CAS messages
and keep the fans operating in flight. • Fixes the fluctuating fuel
temperature indication. • Corrects the calculations to ensure
correct Time to Destination and Time to Go values are presented. •
Corrects the display of the missed approach procedure. • Corrects
failure to intercept DME arc following a go-around. • Corrects most
issues for splits in distance or vertical deviation between the
master and slave FMS that
may sometimes be observed when executing an RNAV approach with a
hold at the IAF and subsequent descent from the holding altitude
constraint to the FAF altitude.
• Corrects the APPR status that is sometimes indicated in the FMS
STATUS field prior to reaching a point 2 nm prior to the FAF on an
approach procedure where ACTIVATE VECTORS has been selected.
• Corrects the vertical deviation pointer that sometimes does not
correctly depict the VGP when approaching the FAF at an angle
greater than the final approach segment angle.
• Corrects the DGR annunciation may be posted on an approach when
all radio navigation aids are deselected, even though the EPU is
less than RNP and HIL is less than HAL.
• Corrects the TOD icon that is occasionally placed incorrectly
with a series of closely spaced waypoints where there is a descent
from the 2nd to 3rd waypoint in a string, and the altitude of the
1st and 2nd waypoints are the same.
• Corrects the issue in the event that a DME arc that exceeded 180°
in duration, there may be an overshoot of the leg following the
arc.
• Corrects the issue and returns the procedures to the database for
continuous 360° turns containing sequential DF-AF legs.
• Corrects the flight plan melding of ARC waypoint issue. •
Corrects the capture from VALT condition. • Corrects the parallel
holding entry issue. • Corrects the APPR annunciation during VOR
approach issue. • Corrects the turn direction on VM legs issue and
returns the procedures to the database. • Corrects the dual reset
on approach issue. • Corrects the wrong turn direction issue. •
Corrects the APPR post during degrade issue. • Corrects the RNP
values issue. • Corrects the radio position source selection issue.
• Corrects the excessive LNAV gain issue. • Corrects the
disappearing flight plan leg issue. • Improvements to reduce the
conditions that can result in vertical deviation indication splits;
however, it is
anticipated that some VNAV deviation splits may still occur. • A
limitation is added to the AFM to prohibit activation of a holding
pattern while on a VPTH descent. • Corrects the wrong turn
following RNP-AR missed approach issue and returns the procedures
to the
database.
HONEYWELL SERVICE INFORMATION LETTERS WEBSITE:
WWW.MYAEROSPACE.COM
Software updates in Epic Phase 5.2 makes corrections to FMS
operation allowing these procedures to be added back into the
Navigation Database and to be used for navigation. Refer to the
Website above for notifications.
Citation ATTACHMENT SB680-34-20
HONEYWELL SIL NUMBER AND TITLE
SIL D201011000003 (Item A) INCORRECT FP MELDING OF ARC WPT AT END
OF STAR AND APPR TRANS. Procedures containing a course change of
180 degrees or more. This excludes holding patterns and procedure
turns, which are flown correctly:
• Last leg of a procedure contains a course change of 180 degrees
or greater. • Last leg has a turn direction specified in the
navigation database. • Last waypoint common in connecting
procedures.
SIL D201011000003 (Item B) MELDING OF ARC WPT AT END OF STAR AND
APPR TRANS. Procedures containing right turn arcs:
• A right turn direction arc leg terminates a procedure (for
example, STAR). • First leg of following procedure (for example,
approach) begins with arc termination. • When arc becomes the
active leg, lateral guidance is incorrect.
SIL D201011000003 (Item C) TURN DIRECTION OF LAST WPT IN DEPARTURE
IS CHANGED IN FP MELDING SID/STAR combinations:
• SID/STAR combinations, which contain common waypoints between
departure, arrival, and/or approach segments. • Course change to
common waypoint is 180 degrees or greater.
SIL D201011000003 (Item D) FMS NOT INTERCEPTING THE ILS Final
approach overshoot
STAR, approach transition and approach contain common
waypoint.
SIL D201011000003 (Item E) FMS/LNAV loss of turn direction on SID
or approach
• Procedures with course change of 180 degrees or greater. •
Altitude terminating leg (displayed on MCDU as *ALT) precedes
course/direct to a fix leg (CF/DF). • Aircraft has reached an
altitude which is above the specified altitude constraint prior to
sequencing the *ALT waypoint. FMS/LNAV loss of turn direction on
SID or approach.
SIL D201011000003 (Item F) Missed approach activation:
• Procedures with course change of 180 degrees or greater. • Any of
the following combinations: track/course/direct to a fix leg
(TF/CF/DF) preceding a CF/DF in a missed approach procedure. • If
missed approach is activated by the pilot on the MCDU, the F MS
will change the turn direction displayed on the MCDU.
SIL D201011000003 (Item G) FLY XXX OR AS ASSIGNED heading
legs:
• Procedures with course change of 180 degrees or greater. •
Heading leg turn direction from database not followed by LNAV. •
FMS will turn in direction of least course change.
SIL D201011000003 (Item I) Continuous 360 turn: • Procedure
containing DF-AF (direct to a fix leg – arc to a fix leg)
combinations • FMS may command a continuous 360 degree turn (left
or right) with no attempt to return to the published
procedure.
FMS 180 DEGREE VM (HEADING) LEGS (SIL D201012000014)
Turn directions on VM legs were not used in LNAV.
FMS TOD MISPLACEMENT (SIL D20101000078) NP:
FMS incorrectly computes TOD when there are 2 level at
constraints.
EARLY SEQ OF ARCS GREATER THAN 180 DEGREES (SIL D201010000079)
NL:
Departure ARC sequences away and LNAV turns wrong way.
DISPLAY OF INCORRECT FMS COURSE LINE ON HSI/MFD (No SIL Required)
FP:
Map display showing a shortcut on MMMX 05 TOLUCA3 departure.
Citation OWNER ADVISORY SB680-34-20
TO:
COMPLIANCE
RECOMMENDED. This service bulletin should be accomplished at a
scheduled maintenance period or phase inspection.
NOTE: For airplanes 680-0291 thru -0323 and airplanes that have
previously complied with the original release of this service
bulletin this service bulletin is mandatory.
NOTE: For airplanes 680-0001 thru -0290 equipped with any EPIC
Phase software prior to 5.0, compliance with this service bulletin
remains recommended.
LABOR HOURS
MATERIAL AVAILABILITY
* Please contact Cessna Service Parts & Programs for current
cost and availability of parts listed in this service bulletin.
Phone at 1-800-835-4000 (Domestic) or 1-316-517-7542
(International). Send email to:
[email protected] or
telefax at 1-316-517-7711.
Based on availability and lead times, parts may require advanced
scheduling.
In cases where the required part(s) are available as exchange,
order the exchange part and, upon completion, expedite the return
of the removed core to avoid return penalties. Contact the Cessna
Service Parts & Programs Sales Desk for availability of
exchange parts.
SB680-34-20 March 15, 2012 Page 1 of 2
Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706,
Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271,
Email:
[email protected]
COPYRIGHT © 2012
Citation OWNER ADVISORY SB680-34-20
WARRANTY
This service bulletin is recommended. Eligible airplanes may
qualify for parts and labor coverage, as described below.
NOTE: For airplanes 680-0291 thru -0323 and airplanes that have
previously complied with the original release of this service
bulletin this service bulletin is mandatory.
Eligibility: All Citations identified within the serial number
effectivity.
Parts Coverage: Cessna-owned and Cessna-authorized Citation Service
Facilities, operators, or other maintenance facilities may submit a
Citation Credit Claim Form for the parts required to accomplish
this bulletin.
Labor Coverage: Cessna-owned and Cessna-authorized Citation Service
Facilities may submit a Citation Credit Claim Form for the labor
necessary to accomplish this service bulletin. Please note Manpower
Requirements for coverage guidelines.
Credit Application:
All work must be completed and the Citation Credit Claim Form
submitted before the date shown below. Send the Citation Credit
Claim, along with any required parts (see Material Information), to
the point of purchase. Parts to be returned to Cessna Service Parts
& Programs should be forwarded to:
Citation Warranty Administration 7121 Southwest Boulevard Wichita,
KS USA 67215
Expiration: June 30, 2014
NOTE: As a convenience, service documents are now available online
to all our customers through a simple, free-of-charge registration
process. If you would like to sign up, please visit the "Customer
Access" link at www.cessnasupport.com to register.
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