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FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 3)*
4-80 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 4)*
510FM-05 AA 4-81
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 5)*
4-82 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 6)*
510FM-05 AA 4-83
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 7)*
4-84 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 8)*
510FM-05 AA 4-85
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 9)*
4-86 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 10)*
510FM-05 AA 4-87
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 11)*
4-88 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 12)*
510FM-05 AA 4-89
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 13)*
4-90 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 14)*
510FM-05 AA 4-91
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 15)*
4-92 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS 15°
(DRY RUNWAY OVER A 35 FOOT SCREEN HEIGHT)
(ANTI-ICE ON)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 4-32. If the runway has a gradient,
adjust V1 and takeoff field length using figure 4-31.
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 4-31*
510FM-05 AA 4-93
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 1 of 15)*
4-94 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 2)*
510FM-05 AA 4-95
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 3)*
4-96 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 4)*
510FM-05 AA 4-97
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 5)*
4-98 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 6)*
510FM-05 AA 4-99
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 7)*
4-100 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 8)*
510FM-05 AA 4-101
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 9)*
4-102 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 10)*
510FM-05 AA 4-103
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 11)*
4-104 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 12)*
510FM-05 AA 4-105
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 13)*
4-106 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-32 (Sheet 14)*
510FM-05 AA 4-107
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-32 (Sheet 15)*
4-108 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
SINGLE-ENGINE TAKEOFF FLIGHT PATH - FLAPS UP
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Citation Mustang airplane flight manual 2(6)
