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7. Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ZERO DIFFERENTIAL
8. Autopilot and Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (at or above minimums)
9. Speed Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT PRIOR TO 50 FEET AGL
10. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VREF
1. Throttle (operating engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE as required
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN VREF
510FM-S6-00 S6-AA S6-5
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 6
FAA APPROVED
U.S. Configuration
ABNORMAL PROCEDURES
No change.
NORMAL PROCEDURES
No change.
PERFORMANCE
Performance data remains the same as the basic Approved Airplane Flight Manual with the following
exceptions.
TAKEOFF
Refer to page S6-7 for procedures for use of takeoff performance tables.
LANDING
Refer to page S6-15 for procedures for use of approach and landing performance tables.
S6-6 S6-AA 510FM-S6-00
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 6
FAA APPROVED
Configuration U.S.
PROCEDURES FOR USE OF TAKEOFF PERFORMANCE
TABLES
1. Determine gross weight of airplane for type of loading desired.
2. Obtain airport information; i.e., active runway, available runway gradient, ambient
temperature (TEMP), altitude, wind, icing conditions and runway gradient (if applicable) and
obstacles in the takeoff flight path. Determine that the temperature is within the ambient
temperature limits found in Section II, OPERATING LIMITATIONS
3. Determine wind component parallel to active runway from the Crosswind Component chart
in Section IV, PERFORMANCE, STANDARD CHARTS.
4. Check the maximum takeoff weight permitted by climb requirements from the Maximum
Takeoff Weight - Pounds Permitted By Climb Requirements tables in Section IV,
PERFORMANCE, TAKEOFF. If this limitation restricts the gross weight, weight must be
reduced until the requirement is met.
5. Using the takeoff weight determined in step 4, determine takeoff field length, V1, VR, V2,
VENR from Figure S6-2.
6. For runway gradients, V1 and takeoff field length must be corrected using the correction
table in Figure S6-1.
7. If the available runway length is less than the required field length, the airplane weight must
be reduced until this requirement can be met.
8. Determine level off altitude. Level off altitude is airport barometric altitude plus takeoff climb
increment required for obstacle clearance from the Single-Engine Takeoff Flight Path
Distances And Takeoff Climb Increment (TCI) tables in Section IV, PERFORMANCE,
TAKEOFF.
9. If the obstacle clearance is a factor, the single-engine takeoff flight path charts in Section IV,
PERFORMANCE, TAKEOFF must be used to determine if the net takeoff flight path
provides the required obstacle clearance. If the required obstacle clearance is not achieved,
the gross weight must be adjusted until the net takeoff flight path assures the required
obstacle clearance.
NOTE
If the takeoff flight path has not been completed within ten (10) minutes, reduce power
to maximum continuous single engine thrust and continue with the takeoff flight path.
10. For second segment and enroute turning climb, up to and including 15° bank angle, if the
takeoff weight is 8352 pounds or less, multiply the takeoff weight by 1.035 to obtain an
adjusted weight. Enter the appropriate Second Segment Takeoff Net Climb Gradient -
Percent or Single Engine Enroute Net Climb Gradient - Percent table in Section IV,
PERFORMANCE, TAKEOFF at the adjusted weight to find the actual climb performance of
the airplane in the bank. If the takeoff weight is greater than 8352 pounds, reduce the net
climb gradient by 0.9
11. The First Segment Takeoff Net Climb Gradient - Percent tables are presented in Section IV,
PERFORMANCE, TAKEOFF.
510FM-S6-00 S6-AA S6-7
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 6
FAA APPROVED
U.S. Configuration
TAKEOFF FIELD LENGTH - FEET
(SOD RUNWAY OVER A 35 FOOT SCREEN HEIGHT)
Determine takeoff field length, V1, VR, V2, and VENR from Figure S6-2. If the runway has a gradient,
adjust V1 and takeoff field length using Figure S6-1.
If the required distance is greater than the available distance, the airplane weight must be reduced
until distance required is less than or equal to distance available.
Figure S6-1
S6-8 S6-AA 510FM-S6-00
MODEL 510 SECTION V - SUPPLEMENTS
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Citation Mustang airplane flight manual 3(6)
