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Pages affected by the current revision are indicated by an asterisk (*) preceding the page number.
Supplement Status Date
Original 11 April 2007
Revision 1 29 August 2007
Revision 2 5 November 2007
Revision 3 18 January 2008
Revision 4 4 March 2008
Revision 5 13 November 2008
LOG OF EFFECTIVE PAGES
Page
Number
Page
Status
Revision
Number
Configuration
Code
* S3-1 thru S3-2 Revised 5 S3-AA
S3-3 Original 0 S3-AA
S3-4 Revised 1 S3-AA
* S3-5 thru S3-6 Revised 5 S3-AA
S3-7 thru S3-8 Original 0 S3-AA
S3-2 S3-AA 510FM-S3-05
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 3
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-S3-00 S3-AA S3-3
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 3
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
S3-AA Airplanes 510-0001 and On using the Citation
Performance Calculator (CPCalc).
S3-4 S3-AA 510FM-S3-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 3
FAA APPROVED
Configuration U.S.
CITATION PERFORMANCE CALCULATOR (CPCALC)
INTRODUCTION
This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for Airplanes 510-0001 and On using performance information from the Citation Performance
Calculator (CPCalc). 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
GENERAL
The software version displayed on the main startup screen of the CPCalc must match the software
version that corresponds with the applicable AFM revision as shown in the following table:
OPERATIONAL APPROVALS
The CPCalc provides FAA approved Section IV Takeoff and Landing performance information and
provides Section VII Wet Takeoff and Landing performance information.
1. The CPCalc is approved for use as an alternative source to the takeoff and landing data
presented in Section IV of the basic FAA Approved Airplane Flight Manual.
2. The CPCalc and AFM are each equally valid sources of performance data; however, the
operator must use speed and distance data from only one of these sources.
3. Inputs with decimal values must be entered into CPCalc using the current decimal separator
symbol selected in the Windows® operating system regional control panel options. No other
separator symbols are allowed as input values.
OPERATING PROCEDURES
The operating procedures are the same as the basic FAA Approved Flight Manual except as follows:
EMERGENCY PROCEDURES
No change.
ABNORMAL PROCEDURES
No change.
NORMAL PROCEDURES
No change.
CPCalc Software Version AFM Revision Temporary Changes
3.X 7 None
510FM-S3-05 S3-AA S3-5
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 3
FAA APPROVED
U.S. Configuration
PERFORMANCE
WARNING
The CPCalc performance that is shown is for those conditions as
specified. Any deviation from these conditions will result in different
performance. There can be combinations of conditions (weight, altitude
and temperature) that could result in performance other than that which
would normally be expected: e.g., as weight gets lighter, required
distances are longer.
DEFINITIONS
NET TAKEOFF FLIGHT PATH METHODS
The airplane is flown to Level Off Altitude per the Gross Takeoff Flight Path. Level Off Altitude is the
sum of Airport Barometric Altitude and Takeoff Climb Increment. The Takeoff Climb Increment is
based on Gross Takeoff Flight Path which is associated with Net Takeoff Flight Path meeting the
requirements of one of the three methods the user specifies. CPCalc provides the level off altitude
and the horizontal distances along the net takeoff flight path. The net takeoff flight path is used to
　
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