Cessna 510 Citation Mustang SERVICE BULLETIN

Citation
SERVICE BULLETIN
SB510-34-14
TITLE
NAVIGATION - GARMIN G1000 SOFTWARE VERSION 010-00435-24 UPGRADE
EFFECTIVITY
MODEL
SERIAL NUMBERS
510 (Citation Mustang)
-0001 thru -0402
The equivalent of this service bulletin has been incorporated on production airplanes -0403 and On.
This service bulletin supersedes SB510-34-11 Navigation - Garmin G1000 Software Version
010-00435-21 Upgrade.
REASON
The 010-00435-24 software provides fixes and enhancements to the Garmin G1000 avionics system.
This service bulletin corrects issues that are defined in the service letters that follow:
•
•
•
SL510-34-17Navigation - Transmittal Of Garmin Service Advisory No. 1101 - GDL 69/69A TFR
(Temporary Flight Restrictions) Reporting Issue
SL510-34-19 Navigation - Transmittal Of Garmin Service Advisory No. 1118 - Momentary Failure
Indications (Red X) Can Occur When Sorting Stored Flight Plans
SL510-34-20 Navigation - Transmittal Of Garmin Service Advisory No. 1129 - Momentary Loss Of GRS
77/77H And GDC 74A/74B/74H Functions
DESCRIPTION
This service bulletin provides parts and instructions to upgrade the Garmin G1000 software to version
010-000435-24.
COMPLIANCE
MANDATORY. This service bulletin must be accomplished by November 15, 2012.
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.
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.
SB510-34-14
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May 4, 2012
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
SERVICE BULLETIN
SB510-34-14
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.
FLIGHT CREW OPERATIONS
Refer to the attached Flight Crew Operations Summary.
WEIGHT AND BALANCE INFORMATION
Negligible
REFERENCES
Cessna Model 510 Maintenance Manual
ICA-510-34-00010 Phase 12 G1000 Software Update ICA Supplement
PUBLICATIONS AFFECTED
Cessna Model 510 FAA Approved Airplane Flight Manual (510FM)
ACCOMPLISHMENT INSTRUCTIONS
1.
Prepare the airplane for maintenance:
A.
2.
(1)
Connect the airplane battery.
(2)
Connect external electrical power.
B.
Move the battery switch to the BATT position.
C.
Move avionics power switch to the AVN PWR position.
Load the Garmin G1000 software to 010-00435-24.
A.
3.
Make sure that all switches are in the OFF/NORM position.
The cards that follow must be available before the software is installed:
•
The 010-00435-24 Garmin SD Card V.435-24.
•
The 010-00330-51 Garmin TAWS unlock card (in the blue software pouch included as loose
equipment at the time of airplane delivery).
•
The 010-00330-50 Garmin ChartView unlock card (in the blue software pouch included as
loose equipment if the ChartView option was purchased at the time of airplane delivery).
•
The 010-00330-55 SVT Unlock Data Card (in the blue software pouch included as loose
equipment if installed).
•
The 010-00435-EO XM Cockpit Unlock Card (in the blue software pouch included as loose
equipment if installed).
Turn on the G1000 in normal mode to verify existing options.
A.
Record the basic empty weight as displayed on the MFD.
B.
Record which options are installed for later reference.
(1)
ADF – Make sure that the softkey 7 on both PFDs is labeled ADF/DME or ADF.
(2)
DME - Make sure that the softkey 7 on both PFDs is labeled ADF/DME or DME.
(3)
TAS – Turn to the MFD MAP – TRAFFIC page. Make sure that the operating mode is NOT TIS.
TIS will have a cyan label in the upper left corner indicating TNA MUTE ON or TNA MUTE OFF.
(4)
HF – Make sure that COM3 is selectable on both audio panels.
(5)
XM in the cockpit - make sure that MUSIC is selectable on both audio panels.
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SERVICE BULLETIN
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SB510-34-14
(6)
C.
ChartView – Turn to the MFD AUX – SYSTEM STATUS page.
(a)
Press the MFD1 DB softkey and use the FMS knob to scroll down to the CHART
database information.
(b)
Make sure that the chart listed is Jeppesen ChartView.
Remove power from the airplane.
CAUTION: Failure to follow the instructions in exact step-by-step order could result in damage to
the GDU SUPPLEMENTAL database and/or SD cards.
4.
Remove and keep the Cessna Diagnostics Maintenance System (CDMS) from the upper slot of the
MFD for later installation.
5.
With all aircraft power off, insert the 010-00435-24 Garmin SD Card V.435-24 into the top card slot of
the PFD 2.
6.
MFD/PFD software load:
A.
Pull the PFD 1, PFD 2, and MFD circuit breakers (primary & secondary).
B.
Move the battery switch to the BATT position.
C.
Move avionics power switch to the AVN PWR position.
D.
Press and hold the bottom right softkey on the PFD 2. Close both PFD 2 circuit breakers to
power on the PFD 2.
E.
Release the softkey after the INITIALIZING SYSTEM message appears.
F.
Press the YES softkey to load GDU system files when the DO YOU WANT TO UPDATE SYSTEM
FILES? prompt appears.
G.
When the software load is complete the message DO YOU WANT TO UPLOAD THE SPLASH
SCREEN will appear. Press the YES softkey at the bottom of the display when the prompt appears.
H.
When the splash screen update is complete you will be asked to PRESS ANY SOFTKEY TO
CONTINUE or allow the auto timer to count down and enter into configuration mode.
NOTE: A UPDATING STANDBY NAVIGATION DATABASE WITH NEWER ACTIVE DATABASE
message will appear on the display. After the database loads the display will verify that the
database loaded correctly.
I.
Software load to the PFD 2 is complete when the display starts into configuration mode.
J.
Leave the display powered on.
K.
Remove the 010-00435-24 Garmin SD Card V.435-24 and insert it into the top MFD slot.
L.
Do Steps 6D thru 6J again for the MFD.
(1)
Use the MFD circuit breakers instead of the PFD 2 circuit breaker.
M.
Remove the 010-00435-24 Garmin SD Card V.435-24 and insert it into the top PFD 1 slot.
N.
Insert the Cessna Diagnostics Maintenance System (CDMS) into the top card slot of the MFD.
NOTE: The Cessna Diagnostics Maintenance System (CDMS) card should remain in the MFD.
O.
Do Steps 6D thru 6J again for PFD 1.
(1)
7.
Use the PFD 1 circuit breakers instead of the PFD 2 circuit breaker.
Initial software load and configuration.
A.
Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1.
B.
Use the small FMS knob to select MUSTANG from the AIRFRAME list and push the ENT softkey.
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SERVICE BULLETIN
SB510-34-14
C.
Turn small FMS knob and scroll down to CESSNA MUSTANG BASE CONFIGURATION and press
enter.
D.
The software included on the 010-00435-24 Garmin SD Card V.435-24 will automatically determine
which files must be loaded.
NOTE: The 010-00435-24 Garmin SD Card V.435-24 may not select files to upload. If this occurs
select clear all and then select all files.
E.
Turn small FMS knob and scroll down to GIA GAINS and press ENT to create a check mark in
that field.
F.
Press the LOAD softkey to load selected software/config items. Periodically monitor the loading
process for failures. A green PASS message is shown beside s/w and config items.
NOTE: Periodically monitor the software load for progress. If the upload to a unit is unsuccessful,
an UPLOAD FAIL message will be posted and the upload will stop. A red FAIL will be
shown beside the software that failed. Press enter to acknowledge the fail message and
to continue the same software load. If unable to load the software after several attempts,
uncheck the software and configuration boxes using the ENT softkey and press the LOAD
softkey to continue with the rest of the software load before troubleshooting cause of failure.
G.
8.
9.
Press the ENT button when all software loading is complete to acknowledge software upload is
complete.
(Airplanes -0001 thru -0379) Load the software configuration.
A.
Use the large FMS knob to go up to the ITEM box.
B.
Select CESSNA MUSTANG OLD NO TCAS II WIRING OPTION from the group list.
C.
Make sure that the GIA 1 and GIA 2 boxes are checked.
D.
Press the LOAD softkey to load selected software/config items. Periodically monitor the loading
process for failures. A green PASS message is shown beside s/w and config items.
E.
Press the ENT button when all software loading is complete to acknowledge software upload is
complete.
F.
Make sure that a green PASS appears next to each loaded item.
G.
Push the UPDT CFG softkey to update the system configuration files.
Enable the DME option:
WARNING:
10.
Do not configure an option that is not installed on the airplane.
A.
Go to Step 10 if the DME option is not installed.
B.
Use the outer FMS knob to move the cursor to the ITEM box.
C.
Use the inner FMS knob to highlight the CESSNA MUSTANG KN-63 DME OPTION from the
group list.
D.
Press the ENT softkey to select the option.
E.
The configuration box for GIA 2, GMA 1, and GMA 2 should be checked.
F.
Press the LOAD softkey to load the DME configuration parameters into GIA 2.
G.
Monitor the configuration load to make sure the green PASS message is next to GIA 2.
H.
Press the ENT button when all software loading is complete to acknowledge software upload is
complete.
Enable the ADF option:
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SERVICE BULLETIN
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WARNING:
11.
A.
Go to Step 11 if the ADF option is not installed.
B.
Use the outer FMS knob to move the cursor to the ITEM box.
C.
Use the inner FMS knob to highlight the CESSNA MUSTANG BECKER ADF OPTION from the
group list.
D.
Press the ENT softkey to select the option.
E.
All configuration boxes should be checked.
•
GIA2
•
GMA1
•
GMA2
F.
Press the LOAD softkey to load all software/config items.
G.
Monitor the configuration load to verify the green PASS message next to each item.
H.
Press the ENT button when all software loading is complete to acknowledge software upload is
complete.
TAS option configuration:
WARNING:
12.
Do not configure an option that is not installed on the airplane.
A.
Go to Step 12 if the TAS option is not installed.
B.
Use the outer FMS knob to move the cursor to the ITEM box.
C.
Use the inner FMS knob to highlight the CESSNA MUSTANG KTA 870 TAS OPTION from the
group list.
D.
Press the ENT softkey to select the option.
E.
The configuration box for GIA 2 should be checked.
F.
Press the LOAD softkey to load the TAS configuration parameters into GIA 2.
G.
Monitor the configuration load to make sure the green PASS message is next to GIA 2.
H.
Press the ENT button when all software loading is complete to acknowledge software upload is
complete.
HF option configuration:
WARNING:
13.
Do not configure an option that is not installed on the airplane.
Do not configure an option that is not installed on the airplane.
A.
Go to Step 13 if the HF option is not installed.
B.
Use the outer FMS knob to move the cursor to the ITEM box.
C.
Use the inner FMS knob to highlight the CESSNA MUSTANG KHF1050 HF OPTION from the
group list.
D.
Press the ENT softkey to select the option.
E.
The configuration box for GMA 1 & 2 should be checked.
F.
Press the LOAD softkey to load the HF configuration parameters into GMA 1 and 2.
G.
Monitor the configuration load to verify the green PASS message next to GMA 1 and 2.
H.
Remove the 010-00435-24 Garmin SD Card V.435-24 from the top slot of the PFD.
I.
Keep the 010-00435-24 Garmin SD Card V.435-24 as loose equipment with the aircraft.
TAWS enable configuration:
A.
Pull the primary and secondary PFD 1 circuit breakers.
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B.
Insert the 010-00330-51 TAWS Unlock Card into the top card slot of PFD 1.
C.
Press and hold the bottom right softkey on the PFD 1.
D.
Push both PFD 1 breakers to power on the PFD 1.
E.
Release the softkey after the INITIALIZING SYSTEM message appears.
F.
Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1.
G.
Push the inner FMS knob to activate the cursor.
H.
Use the inner FMS knob to select CONFIGURATION FILES in the AIRFRAME list and push the
ENT softkey
I.
Use the outer FMS knob to move the cursor to the ITEM box.
J.
Use the inner FMS knob to select the ENABLE TAWS option and push the ENT softkey.
NOTE: When the option is selected the configuration files in the PRODUCT field will be displayed.
K.
Push the CHK ALL softkey to select all files.
L.
Push the LOAD softkey.
M.
Monitor the status of the software upload.
N.
Push the ENT softkey to acknowledge the upload is complete.
O.
Make sure that COMPLETE is displayed in the SUMMARY field.
P.
Push the inner FMS knob to de-activate the cursor.
Q.
Remove the 010-00330-51 TAWS Unlock Card from the display.
NOTE: Once the TAWS unlock card is used to unlock the TAWS on one airplane it cannot be used
to unlock the TAWS on another airplane.
R.
14.
Keep the 010-00330-51 TAWS Unlock Card as loose equipment with the aircraft.
Jeppesen ChartView option configuration:
WARNING:
Do not configure an option that is not installed on the airplane.
A.
Go to Step 15 if the Jeppesen ChartView option is not installed.
B.
Pull the primary and secondary PFD 1 circuit breakers.
C.
Insert the 010-00330-50 ChartView Unlock Card into the top card slot of PFD 1.
D.
Press and hold the bottom right softkey on the PFD 1.
E.
Push both PFD 1 breakers to power on the PFD 1.
F.
Release the softkey after the INITIALIZING SYSTEM message appears.
G.
Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1 .
H.
Push the inner FMS knob to activate the cursor.
I.
Use the inner FMS knob to select CONFIGURATION FILES in the AIRFRAME list and push the
ENT softkey
J.
Use the outer FMS knob to move the cursor to the ITEM box.
K.
Use the inner FMS knob to select the ENABLE CHARTVIEW option and push the ENT softkey.
NOTE: When the option is selected the configuration files in the PRODUCT field will be displayed.
L.
Push the CHK ALL softkey to select all files.
M.
Push the LOAD softkey.
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N.
Monitor the status of the software upload.
O.
Push the ENT softkey to acknowledge the upload is complete.
P.
Make sure that COMPLETE is displayed in the SUMMARY field.
Q.
Push the inner FMS knob to de-activate the cursor.
R.
Remove the unlock card.
NOTE: Once the ChartView unlock card is used to unlock the ChartView on one airplane it cannot
be used to unlock the ChartView on another airplane.
15.
Synthetic Vision System option configuration:
WARNING:
Do not configure an option that is not installed on the airplane.
A.
Go to Step 16 if the Synthetic Vision System option is not installed.
B.
Pull the primary and secondary PFD 1 circuit breakers.
C.
Insert the 010-00330-55 SVT Unlock Data Card into the top slot of PFD 1.
D.
Press and hold the bottom right softkey on the PFD 1.
E.
Push both PFD 1 breakers to power on the PFD 1.
F.
Release the softkey after the INITIALIZING SYSTEM message appears.
G.
Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1.
H.
Push the inner FMS knob to activate the cursor.
I.
Use the inner FMS knob to select CONFIGURATION FILES in the AIRFRAME list and push the
ENT softkey.
J.
Use the outer FMS knob to move the cursor to the ITEM box.
K.
Use the inner FMS knob to select the SVS ENABLE option and push the ENT softkey.
NOTE: When the option is selected the configuration files in the PRODUCT field will be displayed.
16.
L.
Push the CHK ALL softkey to select all files.
M.
Push the LOAD softkey.
N.
Monitor the status of the software upload.
O.
Push the ENT softkey to acknowledge the upload is complete.
P.
Make sure that COMPLETE is displayed in the SUMMARY field.
Q.
Push the inner FMS knob to de-activate the cursor.
R.
Remove the 010-00330-55 SVT Unlock Data Card from PFD 1.
XM cockpit option configuration:
WARNING:
Do not configure an option that is not installed on the airplane.
A.
Go to Step 17 if the XM cockpit option is not installed.
B.
Pull the primary and secondary PFD 1 circuit breakers.
C.
Install the 010-00435-EO XM Unlock Card in the upper slot on the pilot's PFD.
D.
Press and hold the bottom right softkey on the PFD 1.
E.
Close both PFD 1 circuit breakers to power on the PFD.
F.
Release the softkey after the INITIALIZING SYSTEM message appears.
G.
Use the inner FMS knob to go to the SYSTEM UPLOAD PAGE.
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17.
H.
Select MUSTANG from the AIRFRAME list and push the ENT softkey.
I.
Select CESSNA MUSTANG COCKPIT XM OPTION GDU 11.XX & ON from the group list and
push the ENT softkey.
J.
Make sure that the configuration boxes that follow are checked.
•
AIRFRAME
•
GIA2
•
GMA1
•
GMA2
•
ALERTS
K.
Push the LOAD softkey to upload the software.
L.
Monitor the software load and make sure that a green PASS message is displayed.
M.
Remove and keep the 010-00435-EO XM Unlock Card as loose equipment with the aircraft.
Verification:
A.
Move avionics power switch to the OFF position.
B.
Move the battery switch to the OFF position for one minute.
C.
Move the battery switch to the BATT position.
D.
Move avionics power switch to the AVN PWR position.
E.
Make sure that the MSG boxes in both PFDs are empty or only contain the message GPS NAV
LOST if you are in a location without GPS signal.
F.
Make sure that all previously recorded options are functioning properly.
G.
ADF verification, if installed:
•
Make sure that the softkey 7 on both PFDs is labeled ADF/DME or ADF.
•
Make sure that the audio panel ADF buttons work on both GMA.
H.
DME verification, if installed:
•
Make sure that the softkey 7 on both PFDs is labeled ADF/DME or DME.
I.
TAS verification, if installed:
(1)
Turn to the MFD MAP – TRAFFIC page.
(2)
Make sure that the operating mode is NOT TIS.
(3)
The TIS will have a cyan label in the upper left corner indicating TNA MUTE ON or TNA
MUTE OFF.
J.
HF verification, if installed:
•
Make sure that COM3 is selectable on both audio panels.
K.
TAWS verification
L.
(1)
Turn to the MFD MAP – TAWS page.
(2)
TAWS has not been unlocked if a MAP – TERRAIN PROXIMITY page is in its place.
XM in the cockpit, if Installed.
NOTE: A valid XM satellite signal is required to verify the operation of the XM radio.
(1)
Make sure that MUSIC is selectable on both audio panels.
(2)
Push the MUSIC key on the audio control panel
(3)
Use the FMS cursor to select the AUX-XM RADIO page on the MFD.
(4)
Push the VOL softkey on the MFD.
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(5)
Push the VOL + softkey to enable volume control for the XM radio.
NOTE: At every power up the XM radio volume will default to mute.
(6)
M.
N.
Make sure that the XM radio can be heard in the cockpit headsets.
ChartView verification, if installed:
(1)
Turn to the MFD AUX – SYSTEM STATUS page.
(2)
Press the MFD 1 DB softkey and use the FMS knob to scroll down to the CHART database
information.
(3)
Make sure that the chart listed is Jeppesen ChartView.
SVT verification, if installed:
(1)
Press the PFD softkey on the pilot's PFD.
(2)
Press the SYN VIS softkey.
(3)
Make sure that PATHWAY SYN TERR, HRZN HDG, and APT SIGNS are displayed above the
softkeys.
NOTE: The G1000 avionics system must have valid heading values, attitude values, and 3D
GPS position to display the SVT on the PFD.
18.
Do the G1000 system architecture check. (Refer to the Model 510 Maintenance Manual, Chapter 34,
Garmin G1000 Integrated Avionics System - Adjustment/Test.)
19.
Do the AFCS check. (Refer to the Model 510 Maintenance Manual, Chapter 34, Garmin G1000 Integrated
Avionics System - Adjustment/Test.)
20.
Enter the aircraft basic weight on the MFD.
21.
Remove power from the airplane.
22.
Insert the 010-00435-24 Garmin SD Card V.435-24 into the software pouch in the airplane log book.
23.
Make sure the flight crew receives the Flight Crew Operations Summary, which shows the operational
changes that are a result of the accomplishment of this service bulletin.
24.
Make sure that ICA-510-34-00010 Phase 12 G1000 Software Update ICA Supplement is available
for future maintenance.
25.
Record that this service bulletin has been completed.
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 East 34th Street North, Building 1600 Suite 1607 Wichita, KS 67226.
MATERIAL INFORMATION
Order the kit below to install this modification.
NEW P/N
QUANTITY
KEY WORD
OLD P/N
INSTRUCTIONS/
DISPOSITION
SB510-34-14
1
Kit, consisting of the following
parts:
010-00435-24
1
Garmin SD Card V.435-24
010-00435-16
Discard
190-00600-04
1
Cockpit Reference Guide
190-00600-03
Discard
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ATTACHMENT
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GARMIN G1000 SOFTWARE CONFIGURATION
CONTROL
SOFTWARE
PART
NUMBER
PRODUCTION
EFFECTIVITY
SERVICE
BULLETIN
EFFECTIVITY
SERVICE
BULLETIN
SERVICE
BULLETIN
COMPLIANCE
REPLACES
SOFTWARE
PART
NUMBER
01000435-09
-0001 thru -0065
Not Applicable
Not Applicable
Not Applicable
Not Applicable
01000435-10
-0066 thru -0152
-0001 thru -0065
SB510-34-02
Mandatory
010-00435-09
01000435-13
-0153 thru -0177
Not Applicable
Not Applicable
Not Applicable
010-00435-10
01000435-16
-0178 thru -0371
-0001 thru -0177
SB510-34-09
Recommended 010-00435-13
01000435-21
-0372 thru -0402
-0001 thru -0371
SB510-34-11
Mandatory
010-00435-16
01000435-24
-0403 and On
-0001 thru -0402
SB510-34-14
Mandatory
010-00435-21
ATTACHMENT
Citation
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LRU SOFTWARE AND VERSION
LINE REPLACEABLE UNIT
(LRU)
SOFTWARE PART NUMBER
VERSION
COM1
006-B0081-XX
7.00 or 10.00
COM2
006-B0081-XX
7.00 or 10.00
GCU
006-B0387-20
3.00
GDC1
006-B0261-18
3.08
GDC1FPGA
006-C0055-00
1.05
GDC2
006-B0261-18
3.08
GDC2FPGA
006-C0055-00
1.05
GDL69
006-B0317-21
4.01
GEA1
006-B0193-05
2.07
GEA2
006-B0193-05
2.07
GFC CERT GIA1
006-D0356-15
2.06
GFC CERT GIA2
006-D0356-15
2.06
GFC CERT P C
006-D0356-15
2.06
GFC CERT P M
006-D0356-15
2.06
GFC CERT PT C
006-D0356-15
2.06
GFC CERT PT M
006-D0356-15
2.06
GFC CERT R C
006-D0356-15
2.06
GFC CERT R M
006-D0356-15
2.06
GFC CERT Y C
006-D0356-15
2.06
GFC CERT Y M
006-D0356-15
2.06
GIA 1
006-B0544-38
6.40
GIA 1 AUDIO
006-D0425-06
2.11
GIA 2
006-B0544-38
6.40
GIA 2 AUDIO
006-D0425-06
2.11
GMA1
066-B0203-43
4.03
GMA2
066-B0203-43
4.03
GMC
066-B0387-20
3.00
GMU1
006-B0224-01
2.05
GMU1 FPGA
006-C0048-00
2.00
GMU2
006-B0224-01
2.05
ATTACHMENT
Citation
SB510-34-14
LINE REPLACEABLE UNIT
(LRU)
SOFTWARE PART NUMBER
VERSION
GMU2 FPGA
006-C0048-00
2.00
GPS1
006-B0339-0A
3.2
GPS2
006-B0339-0A
3.2
GRS1
006-B0223-22
3.02
GRS1 FPGA
006-C0049-00
2.00
GRS1 MV DB
006-D0159-01
2xxx (*)
GRS 2
006-B0223-22
3.02
GRS2 FPGA
006-C0049-00
2.00
GRS2 MV DB
006-D0159-01
2xxx (*)
GS1
006-B0083-XX
4.00 or 6.01
GS2
006-B0083-XX
4.00 or 6.01
GSA PTCH CTL
006-B0398-32
2.30
GSA PTCH MON
006-B0398-32
2.30
GSA PTCH TRIM C
006-B0398-32
2.30
GSA PTCH TRIM M
006-B0398-32
2.30
GSA ROLL CTL
006-B0398-32
2.30
GSA ROLL MON
006-B0398-32
2.30
GSA YAW CTL
006-B0398-32
2.30
GSA YAW MON
006-B0398-32
2.30
GTX1
006-B0172-XX
6.11
GTX2
006-B0172-XX
6.11
GWX
006-B0266-10
2.11
GWX FPGA
006-C0042-06
3.01
MFD1
006-B0319-A3
12.03
MFD1 FPGA
006-C0036-04
1.04
NAV1
006-B0082-XX
5.01, 5.02, 5.03, or 6.01
NAV2
006-B0082-XX
5.01, 5.02, 5.03, or 6.01
PFD1
006-B0319-A3
12.03
PFD1 FPGA
006-C0036-04
1.04
PFD2
006-B0319-A3
12.03
PFD2 FPGA
006-C0036-04
1.04
(*) The GRS RGF is updated every five years. 2xxx defines the current year.
Citation
ATTACHMENT
SB510-34-14
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 is informational only and does not supersede any information in the FAA-approved
airplane flight manual.
•
XM Weather: NEXRAD and Icing/Turbulence is mutually exclusive on weather datalink page. Icing and
Turbulence may be shown together, but NEXRAD will be turned off when either are enabled. When
NEXRAD is enabled by the pilot, both Icing and Turbulence will be turned off.
•
Garmin Display Unit: Added a Selected Altitude Intercept Arc to the following moving maps: main
Navigation map, PFD inset map, AUX - Trip Planning map, Active Flight Plan page map, and all NRST
maps. A cyan arc shall be drawn on the map (when enabled via the Map Setup menu and not suppressed)
to indicate the location at which the aircraft will reach the selected altitude based on current barometric
altitude, vertical speed, and ground speed. The arc is drawn along the aircraft's current track.
•
The main NAV map page's profile view, which shows the airplane's vertical position over the terrain
and obstacles along a swath centered on the current airplane ground track. When datalink weather is
available, winds aloft information is also shown which depicts headwind or tailwind as a function of
altitude. This vertical profile view is turned on or off via the PROFILE softkey under the MAP sub-tier of
softkeys. This feature is only available if specifically enabled in the airframe configuration.
•
Flight Planning Improvements: If the VECTORS transition is chosen when an approach is loaded,
or if ACTIVATE VECTOR-TO-FINAL is selected from the PROC menu, waypoints from one of the
transitions that are near the course to the final approach fix will be loaded into the approach, however the
course-to-fix leg to the FAF will still become the active leg when VTF is activated. The other waypoints will
be loaded into the flight plan and shown on the map. In this case a gap will be inserted ahead of the
first leg of the approach, so that if the pilot allows leg sequencing into the approach to occur, it will start
with the first leg contained completely in the approach rather than connecting a leg from the last en route
waypoint to the first waypoint of the approach.
•
Flight Planning Enhancements:
•
Added configurable options to improve waypoint insertion on the active flight plan page
•
A hollow box can be drawn with a dashed outline around the selected field, a precursor. When the
precursor is enabled, functions that required the cursor to be active will work as though the cursor
was active. For example, alphanumeric key will automatically start inserting a waypoint at the
indicated location or edit the currently selected field.
•
An arrow can also be drawn indicating where in the current flight plan a new waypoint would be
inserted based on the currently selected field.
•
The selected field (precursor or cursor) can be adjusted by using the joystick when it is not being
used to pan the map. Pushing the joystick up moves the selection up a row while pushing the
joystick down moves it down a row. Pushing the joystick right will move the selection right to the
next highlightable column or down to the next row if the last column in the row is currently selected.
Pushing the joystick to the left will move the selection left to the next highlightable column or up to
the next row if the first column in the row is currently selected.
•
The blank entry can be selected the first time the active flight plan page is opened after a power-up
rather than the first waypoint in the list.
•
Each of these improvements can be configured independently and are disabled unless configured
by the airframe.
•
Graphical Weather Enhancements:
•
Added the display of graphical METARs to the moving maps and to the active flight plan page.
Added the display of the raw METAR text to the active flight plan page and the moving maps (when
highlighting the METAR flag with the map cursor). Added the display of a weather legend to maps
that share the weather related softkeys (NEXRAD, XM LTNG, METAR). The legend is accessible via
the LEGEND softkey in the MAP tier. The active flight plan page can be configured to show METAR
Citation
ATTACHMENT
SB510-34-14
•
•
•
•
•
•
•
•
flags/reports from nearby reporting stations for waypoints in the flight plan without an active reporting
station. The search radius is configurable from 0-99 NM, the Model 510 has a 30 NM search radius.
•
Decoded wind direction in METARs is now always reported as a three digit number to avoid any
confusion (20 could be interpreted as 200 or 020).
•
Added time to decoded display of METAR on waypoint airport weather page. The METAR
observation time was previously shown in the raw METAR text on the WPT-WEATHER
INFORMATION page for airports. To assist the pilot in quickly determining the relevance of the
observation, the "decoded METAR observation time" and the "elapsed time since the observation"
have been added to the page.
•
The time displayed for temporary flight restrictions (TFRs) now includes a reference to the time
format selected by the pilot on the SYSTEM SETUP page. When UTC time is selected, the TFR will
include a suffix of UTC. When Local 24hr time is selected, the TFR time will include a suffix of LCL.
When Local 12hr time is selected, the TFR time will include a suffix for AM/PM.
•
The logic to display the text of a METAR in yellow when it is more than 75 minutes old was removed
so the color remains constant at all times. Also, METAR parsing logic was updated to correctly
convert the altimeter field from HPA to inches of mercury.
•
Default corners for TFR boundary box were changed to include Eastern/Southern hemisphere
points. Longitudinal correction was fixed when parsing arc shaped TFR's. Reference Garmin
Service Advisory SA-1101.
Radio Altimeter Display Location Improvement: Moved the locations of Radio Altitude Height and Radio
Altitude Test Status. When the "RA" label is configured to be displayed adjacent to the Radio Altitude
Height, the text sizing and coloration has changed for the "RA" label to harmonize with labels used
elsewhere.
SVT Improvement: SVT will now determine if a runway highlight should be rendered. If there is terrain
between the current aircraft position and the runway, that would obscure the runway, then the highlight
will not be displayed.
Altitude Labeling Improvements:
•
Changed labeling according to AC 20-163 recommendation that systems display GPS geometric
altitude relative to sea level using a label of "GSL" to denote information and prevent possible
confusion.
•
This change applies to the MAP - TERRAIN PROXIMITY or MAP - TAWS page and the AUX - GPS
STATUS page. The terrain/TAWS page has changed from 'GPS ALT MSL' to 'GPS ALT GSL' and
the AUX - GPS STATUS page has changed from 'ALTITUDE' to 'ALT GSL'.
Altitude Select Knob Enhancement: Added support for configurable acceleration on the altitude select
(ALT SEL) knob.
Standby Navigation Database Improvement: The standby navigation database loading function was
modified to remove manual control of the DB SYNC function. Additionally the Garmin logo startup screen
was modified to display a notification "Please Wait. Navigation Database Update in Progress. Do Not
Remove Power from Displays." when a transfer occurs on startup to prevent the startup delay from causing
concern. Updating the active navigation database in a GDU will also update the standby navigation
database in the same GDU. Note, manual updates of the active navigation database must be performed
on each GDU. With this Improvement the Standby Navigation Database Feature will be enabled on.
Flight Plan Sorting Removed: The functionality that allowed sorting the stored flight plans was removed.
New System Message:
•
When the intercept angle between heading and the armed NAV signal (LOC) exceeds 105 degrees
of angular deviation, capture of the armed signal is suppressed. After the suppression logic is
activated, the FD will not capture the signal until the angular deviation becomes 100 degrees or less.
•
This change incorporates a system message if the LOC cannot capture due to the intercept angle
being greater than 105 degrees. The message is “NO NAV CAPTURE - Intercept angle too large for
LOC/BC”
•
If the LOC mode will not capture due to an intercept angle greater than 105 degrees, then a
message or indication should be provided to the pilot. (similar to how the VNAV mode provides
messages and indications if there is something wrong).
Vertical Constraints Improvement: All vertical constraints prior to the active vertical waypoint are now
removed from the active flight plan when baro-VNAV is disabled by the pilot. As a result disabling and
re-enabling baro-VNAV provides another way (in addition to modifying the FPA, the VS TGT, or initiating
a vertical direct-to) to override the effects of any prior vertical constraint and quickly command the
baro-VNAV system to base the computed vertical descent on only the current aircraft location and the
Citation
ATTACHMENT
SB510-34-14
•
next valid vertical constraint ahead of the aircraft. Note that this change to the vertical flight plan may also
affect pathways in some systems that incorporate this navigation library.
GFC Transitioning Improvement: Previously when an ILS approach with VECTORS transition was loaded
and the FAF waypoint became active due to automatic leg sequencing the CDI immediately switched
from GPS to LOC as designed. However, if this automatic transition occurred when the GFC 700 was
GPS-coupled, it would cancel the GPS-coupled mode and transition to wings-level (ROL) mode. In
GDU software version 11.10, the behavior of VECTORS transitions was changed to include waypoints
before the FAF, making it more likely for the FAF to become active due to automatic leg sequencing
while flying GPS-coupled. For example, flying direct to one of these approach waypoints prior to the
FAF will result in the FAF eventually becoming active as a result of automatic leg sequencing. This
change allows the autopilot to remain GPS-coupled until the LOC is captured seamlessly, rather than
reverting to wings-level (ROL) mode, when an automatic GPS to ILS source change occurs as a result of
automatically sequencing to a VECTORS transition.
OWNER ADVISORY
Citation
SB510-34-14
TITLE
NAVIGATION - GARMIN G1000 SOFTWARE VERSION 010-00435-24 UPGRADE
TO:
Cessna Aircraft Owner
REASON
The 010-00435-24 software provides fixes and enhancements to the Garmin G1000 avionics system.
This service bulletin corrects issues that are defined in the service letters that follow:
•
•
•
SL510-34-17Navigation - Transmittal Of Garmin Service Advisory No. 1101 - GDL 69/69A TFR
(Temporary Flight Restrictions) Reporting Issue
SL510-34-19 Navigation - Transmittal Of Garmin Service Advisory No. 1118 - Momentary Failure
Indications (Red X) Can Occur When Sorting Stored Flight Plans
SL510-34-20 Navigation - Transmittal Of Garmin Service Advisory No. 1129 - Momentary Loss Of GRS
77/77H And GDC 74A/74B/74H Functions
COMPLIANCE
MANDATORY. This service bulletin must be accomplished by November 15, 2012.
LABOR HOURS
WORK PHASE
MAN-HOURS
Modification
3.5
MATERIAL AVAILABILITY
PART NUMBER
AVAILABILITY
COST
SB510-34-14
*
*
* 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.
The customer will be responsible for the cost of parts and labor if this service bulletin is completed
after November 15, 2012.
SB510-34-14
Page 1 of 2
May 4, 2012
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
SB510-34-14
WARRANTY
This bulletin is mandatory. Eligible airplanes may qualify for parts and labor coverage, as described below.
Eligibility:
All Citations identified within the serial number effectivity of this service bulletin.
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:
December 31, 2012
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.
SB510-34-14
Page 2
May 4, 2012