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510FM-06 AH 4-69
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 9)*
4-70 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 10)*
510FM-06 AH 4-71
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 11)*
4-72 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 12)*
510FM-06 AH 4-73
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 13)*
4-74 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 14)*
510FM-06 AH 4-75
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 15)*
4-76 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS UP
(DRY RUNWAY OVER A 35 FOOT SCREEN HEIGHT)
(ANTI-ICE ON)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 4-28. If the runway has a gradient,
adjust V1 and takeoff field length using figure 4-27.
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 4-27
510FM-06 AI 4-61.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 1 of 15)
4-62.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 2)
510FM-06 AI 4-63.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 3)
4-64.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 4)
510FM-06 AI 4-65.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 5)
4-66.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 6)
510FM-06 AI 4-67.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 7)
4-68.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 8)
510FM-06 AI 4-69.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 9)
4-70.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 10)
510FM-06 AI 4-71.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 11)
4-72.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 12)
510FM-06 AI 4-73.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 13)
4-74.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 14)
510FM-06 AI 4-75.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 15)
4-76.1 AI 510FM-06
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 OFF)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 4-30. If the runway has a gradient,
adjust V1 and takeoff field length using figure 4-29.
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 4-29*
510FM-05 AA 4-77
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-30 (Sheet 1 of 15)*
4-78 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-30 (Sheet 2)*
510FM-05 AA 4-79
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
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Citation Mustang airplane flight manual 2(5)
