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situational awareness information. It is not intended as a means for navigation or flight
guidance. The aircraft symbol is not to be used for conducting instrument approaches
or departures, and it should not be relied upon during low visibility taxi operations.
Position accuracy, orientation, and related guidance must be assured by other means
of required navigation.
2. Operators must have back-up charts available to the flight crew.
3. Database currency must be verified prior to use via database effectivity page.
4. The flight crew is responsible for verifying availability of charts for the planned flight.
OPERATING PROCEDURES
The operating procedures are the same as those in the basic FAA Approved Airplane Flight Manual
except as follows:
EMERGENCY PROCEDURES
No change.
ABNORMAL PROCEDURES
The Garmin FliteCharts and the Jeppesen ChartView System features are not available when the
MFD or PFD is in the reversion mode.
NORMAL PROCEDURES
No change.
510FM-S01-00 S01-AA S01-5
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 01
FAA APPROVED
U.S. Configuration
PERFORMANCE
No change.
DESCRIPTION
The Garmin FliteCharts or the Jeppesen ChartView System allows display of Jeppesen charts on the
MFD. On applicable charts, the airplane position is shown on the chart with a magenta symbol.
Database effectivity is shown on the MFD power-up page. Databases that are out of date are shown
in amber.
Backup charts must be available to the flight crew when using FliteCharts or ChartView as the
primary chart reference.
For additional information, refer to the Garmin G1000 Cockpit Reference Guide for the Cessna
Citation Mustang or the Garmin G1000 Integrated Flight Deck Pilot’s Guide, Cessna Citation
Mustang.
S01-6 S01-AA 510FM-S01-00
U.S.
MODEL 510
510-0001 AND ON
SUPPLEMENT 2
24 APRIL 2007
REVISION 2 28 JANUARY 2008 S2-1
COPYRIGHT © 2007
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
510FM-S2-02
STEEP APPROACH OPERATIONS
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 2
FAA APPROVED
U.S. Configuration
SUPPLEMENT 2
STEEP APPROACH OPERATIONS
Use the Log of Effective Pages to determine the current status of this supplement.
Pages affected by the current revision are indicated by an asterisk (*) preceding the page number.
Supplement Status Date
Original 24 April 2007
Revision 1 14 September 2007
Revision 2 28 January 2008
LOG OF EFFECTIVE PAGES
Page
Number
Page
Status
Revision
Number
Configuration
Code
* S2-1 thru S2-2 Revised 2 S2-AA
S2-3 Original 0 S2-AA
S2-4 thru S2-5 Revised 1 S2-AA
S2-6 thru S2-10 Original 0 S2-AA
* S2-11 thru S2-22 Revised 2 S2-AA
S2-2 S2-AA 510FM-S2-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 2
FAA APPROVED
Configuration U.S.
SERVICE BULLETIN CONFIGURATION LIST
The following is a list of Service Bulletins that are applicable to the operation of the airplane, and
have been incorporated into this supplement. This list contains only those Service Bulletins that are
currently active.
Number Title Airplane Serial
Effectivity
Revision
Incorporated
Incorporated
in Airplane
510FM-S2-00 S2-AA S2-3
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 2
FAA APPROVED
U.S. Configuration
AIRPLANE CONFIGURATION CODES
The following is a list of airplane configuration codes which appear at the bottom of each page of this
supplement to the basic FAA Approved Airplane Flight Manual, and indicate page effectivity by serial
number. This list contains only the configurations which have been incorporated into this
supplement.
Configuration
Code
Effectivity by
Serial Number
S2-AA Airplanes 510-0001 and On.
S2-4 S2-AA 510FM-S2-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 2
FAA APPROVED
Configuration U.S.
STEEP APPROACH OPERATIONS
INTRODUCTION
This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for Airplanes 510-0001 and On. The information contained herein supplements the information of the
basic FAA Approved Airplane Flight Manual and is applicable when conducting approaches with
approach glidepath angles from 4.5° up to and including 5.5°. For limitations, procedures and
performance information not contained in this supplement, consult the basic FAA Approved Airplane
Flight Manual.
OPERATING LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITATIONS
Normal AFM center of gravity and weight limits apply.
　
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