COPYRIGHT © 2006
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
510CLNP-07
30 AUGUST 2006
THIS CHECKLIST IS CURRENT WITH MODEL 510
CITATION MUSTANG (510-0001 AND ON) FAA APPROVED
U.S. AIRPLANE FLIGHT MANUAL REVISION 7 DATED
21 NOVEMBER 2008. (PART NUMBER 510FM-07)
the best safety device in any aircraft is a well trained crew....
REVISION 7 21 NOVEMBER 2008
Configuration
INTRODUCTION MODEL 510
NOTICE
THE PILOTS’ ABBREVIATED CHECKLIST EXCLUDES NOTES AND
SYSTEM DESCRIPTIONS FOUND IN THE FAA APPROVED AIRPLANE
FLIGHT MANUAL; THEREFORE, IT SHOULD NOT BE USED UNTIL
THE FLIGHT CREW HAS BECOME FAMILIAR WITH THE AIRPLANE,
ITS SYSTEMS, AND THE FAA APPROVED AIRPLANE FLIGHT
MANUAL. SHOULD ANY CONFLICT EXIST BETWEEN THE
ABBREVIATED CHECKLIST AND THE CHECKLIST IN THE FAA
APPROVED AIRPLANE FLIGHT MANUAL, THE FLIGHT MANUAL
SHALL TAKE PRECEDENCE. ALL AIRPLANE FLIGHT MANUAL
NORMAL, EMERGENCY AND ABNORMAL PROCEDURE ITEMS MUST
BE ACCOMPLISHED REGARDLESS OF WHICH CHECKLIST IS USED.
LOG OF EFFECTIVE PAGES
Use this page to determine the currency and applicability of your Pilots’
Abbreviated Checklist. Pages affected by the current revision are
indicated by an asterisk (*) preceding the pages listed under the Page
Number column. Refer to page iv for configuration code definitions, then
determine which pages are applicable to your airplane under the
configuration code column.
Following is a description of the Log of Effective Pages columns:
Page Number . . . . . . . . . .Pilots’ Abbreviated Checklist page number.
Page Status . . . . . . . . . . . . Indicates if the page has been added,
revised or deleted by the current revision.
Revision Number . . . . . . . . . . . . . . .Indicates the revision number.
Configuration Code. . .Indicates page effectivity by two letter code.
REVISION NUMBER DATE
Original 30 August 2006
Revision 1 27 October 2006
Revision 2 30 November 2006
Revision 2A 31 January 2007
Revision 3 7 February 2007
Revision 4 13 April 2007
Revision 5 02 November 2007
Revision 6 29 February 2008
Revision 7 21 November 2008
PAGE
NUMBER
PAGE
STATUS
REVISION
NUMBER
CONFIGURATION
CODE
* Title Revised 7 AA
* ii thru iv Revised 7 AA
* v/vi Added 7 AA
1 Revised 6 AA
2 Original 0 AA
3 Revised 5 AA
* 4 Revised 7 AA
5 Revised 5 AA
ii AA 510CLNP-07
Configuration
MODEL 510 INTRODUCTION
PAGE
NUMBER
PAGE
STATUS
REVISION
NUMBER
CONFIGURATION
CODE
6 Revised 6 AA
* 7 Revised 7 AA
* 8 Revised 7 AJ
* 8.1 Added 7 AK
* 9 thru 11 Revised 7 AA
12 thru 14 Revised 5 AA
15 thru 19 Revised 6 AH
15.1 thru 19.1 Added 6 AI
20 Revised 5 AA
21 thru 25 Revised 6 AH
21.1 thru 25.1 Added 6 AI
26 thru 37 Revised 5 AA
* 38 Revised 7 AA
39 Revised 5 AA
* 40 Revised 7 AA
41 thru 47 Revised 5 AA
48 Revised 6 AF
48.1 Revised 6 AG
49 thru 56 Revised 5 AA
57 thru 58 Revised 6 AA
* 59 Revised 7 AJ
* 59.1 Added 7 AK
* 60 Revised 7 AA
510CLNP-07 AA iii
Configuration
INTRODUCTION MODEL 510
CHECKLIST PART NUMBER
Each page in this checklist contains the part number of the checklist and
the page status of each page. Refer to the following example:
CONFIGURATION CODES
The following is a list of configuration codes which appear at the bottom of
each page of the Pilots’ Abbreviated Checklist and indicate page
effectivity by serial number. Pages marked AA apply to all airplanes of this
model. This list contains only the configurations which have been
incorporated into this checklist.
Each page of the checklist is provided with a configuration code. In the
event that a page is applicable to only a select number of airplanes, at
least two (2) pages will be provided, one with a regular page number (e.g.,
15), and one with a point page number (e.g., 15.1). The operator must
then check the configuration code list in the front of the checklist to
determine which page applies to his/her airplane. In some cases, multiple
pages may be provided to allow for all configurations. This system allows
for a “custom” checklist for each individual aircraft and therefore
eliminates material that does not apply to the operator’s airplane from the
checklist. The page(s) that does(do) not apply to the airplane must be
discarded. From each grouping, identify and record the configuration code
that applies to your airplane, then select and insert the correct pages into
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