Citation Mustang airplane flight manual 2(21)

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plan obstacle clearance. CPCalc will reduce the gross weight, if necessary, to meet specific flight
path performance requirements. CPCalc provides three methods for the user to specify net takeoff
flight path performance.
1. The net takeoff flight path will level off at a fixed height 1500 feet above the takeoff surface.
Figure S3-1
(Continued Next Page)
Climb Gradient Surface: Imaginary surface located 35 feet above the end of the
available runway and inclined at a required gradient.
S3-6 S3-AA 510FM-S3-05
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 3
FAA APPROVED
Configuration U.S.
PERFORMANCE (Continued)
2. The net takeoff flight path may continue the 2nd segment climb beyond 1500 feet to clear an
obstacle located anywhere along the path by at least 35 feet.
Figure S3-2
3. The net takeoff flight path may continue the 2nd segment climb beyond 1500 feet until the
aircraft reaches an assigned level off altitude. The net takeoff flight path is prevented from
penetrating a defined climb gradient surface.
Figure S3-3
510FM-S3-00 S3-AA S3-7
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 3
FAA APPROVED
U.S. Configuration
DESCRIPTION
SOFTWARE PROCEDURES
The CPCalc software provides help with detailed information on how to use the CPCalc for
calculating Takeoff and Landing performance information.
1. Operational landing distance factor requirements may be set under the menu selection
ToolsOptions, or the keyboard shortcut CTRL+O.
2. Climb Gradient calculator is available under the menu selection ToolsClimb Gradient
Calculator, or the keyboard shortcut CTRL+G.
3. Help is available under the menu selection HelpContents. For help specific to the screen
shown, press the F1 key.
4. The calculated performance data may be printed to a connected printer by selecting the
Print All Takeoff or Print All Landing buttons on the appropriate output tabs.
5. Additional condition information is available from each output tab by selecting the
Additional Conditions button or the keyboard shortcut Alt+C.
SOFTWARE INFORMATION
1. The CPCalc software has been demonstrated to function with the following Microsoft®
Windows® operating system versions:
2. The CPCalc software has been demonstrated to work with the following personal computer
processors:
3. It is recommended that CPCalc be installed on a system that meets the following system
requirements:
• Microsoft® Windows® operating system (98, ME, NT, 2000, XP, Vista).
• Minimum CPU 300 MHz, recommended CPU 600 MHz or better (Intel® or AMD®).
• Minimum memory 64 MB, recommended memory 128 MB or higher.
• 30 MB free disk space for installation.
• Desktop, laptop, or tablet PC with CD-ROM drive for installation.
• Input device (keyboard/mouse/pen).
• Display that supports a resolution of 800 x 600 at 96 DPI or, 1024 x 768 at 120 DPI.
• Administrative rights to install programs.
• Microsoft® Data Access Components (MDAC) Version 2.5 or higher (included on
installation CD).
Microsoft®
Windows® 98 SP1, 98SE, or ME
Windows® NT® 4.0 SP4, SP6
Windows® 2000 SP3
Windows® XP SP1,SP2
Windows® Vista®
Intel® AMD®
Pentium® II
Pentium® III
Pentium® 4
K6®
Athlon XP
S3-8 S3-AA 510FM-S3-00
U.S.
MODEL 510
510-0001 AND ON
SUPPLEMENT 4
EASA CERTIFIED AIRPLANES
18 JULY 2007
REVISION 2 4 DECEMBER 2008 S4-1
COPYRIGHT © 2007
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
510FM-S4-02
This Airplane Flight Manual Supplement is approved by the U.S. Federal Aviation Administration
(FAA) on behalf of the European Aviation Safety Agency (EASA).
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
SUPPLEMENT 4
EASA CERTIFIED 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 18 July 2007
Revision 1 4 December 2008
Revision 2 4 December 2008
LOG OF EFFECTIVE PAGES
Page
Number
Page
Status
Revision
Number
Configuration
Code
* S4-1 thru S4-4 Revised 2 S4-AA
S4-5 Original 0 S4-AA
S4-6 thru S4-8 Revised 1 S4-AA
* S4-9 thru S4-24 Revised 2 S4-AH
* S4-9.1 thru S4-24.1 Added 2 S4-AI
* S4-25 thru S4-40 Revised 2 S4-AH
* S4-25.1 thru S4-40.1 Added 2 S4-AI
　
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