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MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 10
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
SB510-34-02 Navigation - Hardware
and Software Update for
Garmin G1000 Avionics
510-0001 thru
-0065
1
510FM-S10-02 S10-AA S10-3
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 10
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. The codes 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
S10-AA 510-0001 and On equipped with the Iridium SATCOM
Antenna.
S10-AB 510-0001 thru -0065 incorporating SB510-34-02,
Navigation - Hardware and Software Update for Garmin
G1000 Avionics, and 510-0066 and On.
S10-AC 510-0001 thru -0065 not incorporating SB510-34-02,
Navigation - Hardware and Software Update for Garmin
G1000 Avionics.
S10-4 S10-AA 510FM-S10-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 10
FAA APPROVED
Configuration U.S.
IRIDIUM SATCOM ANTENNA
INTRODUCTION
This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for airplanes equipped with the Iridium SATCOM Antenna. The information contained herein
supplements the information of the basic FAA Approved Airplane Flight Manual. For limitations,
procedures and performance information not contained in this supplement, consult the basic FAA
Approved Airplane Flight Manual.
OPERATING LIMITATIONS
Maximum Iridium SATCOM transmit power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . <7 Watts
Iridium SATCOM operating frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1616 – 1626.5 MHZ
OPERATING PROCEDURES
The operating procedures are the same as those in the basic FAA Approved Airplane Flight Manual.
EMERGENCY PROCEDURES
No change.
ABNORMAL PROCEDURES
No change.
NORMAL PROCEDURES
No change.
PERFORMANCE
No change.
510FM-S10-01 S10-AB S10-5/S10-6
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 10
FAA APPROVED
Configuration U.S.
IRIDIUM SATCOM ANTENNA
INTRODUCTION
This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for airplanes equipped with the Iridium SATCOM Antenna. The information contained herein
supplements the information of the basic FAA Approved Airplane Flight Manual. For limitations,
procedures and performance information not contained in this supplement, consult the basic FAA
Approved Airplane Flight Manual.
OPERATING LIMITATIONS
Maximum Iridium SATCOM transmit power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . <7 Watts
Iridium SATCOM operating frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1616 – 1626.5 MHZ
Navigation based solely on GPS is prohibited during Iridium SATCOM operations. Alternate primary
means of navigation should be selected prior to Iridium SATCOM use.
OPERATING PROCEDURES
The operating procedures are the same as those in the basic FAA Approved Airplane Flight Manual.
EMERGENCY PROCEDURES
No change.
ABNORMAL PROCEDURES
No change.
NORMAL PROCEDURES
No change.
PERFORMANCE
No change.
510FM-S10-02 S10-AC S10-5.1/S10-6.1
U.S.
MODEL 510
510-0001 AND ON
SUPPLEMENT 12
JAPANESE REGISTERED AIRPLANES
10 SEPTEMBER 2008
S12-1
COPYRIGHT © 2008
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
510FM-S12-00
FAA APPROVED ON BEHALF OF THE JAPAN CIVIL AVIATION BUREAU (JCAB)
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 12
FAA APPROVED
U.S. Configuration
SUPPLEMENT 12
JAPANESE REGISTERED AIRPLANES
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 10 September 2008
LOG OF EFFECTIVE PAGES
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