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TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 14)*
510FM-06 AH 4-59
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 15)*
4-60 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 OFF)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 4-26. If the runway has a gradient,
adjust V1 and takeoff field length using figure 4-25.
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 4-25
510FM-06 AI 4-45.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 1 of 15)
4-46.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 2)
510FM-06 AI 4-47.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 3)
4-48.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 4)
510FM-06 AI 4-49.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 5)
4-50.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 6)
510FM-06 AI 4-51.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 7)
4-52.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 8)
510FM-06 AI 4-53.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 9)
4-54.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 10)
510FM-06 AI 4-55.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 11)
4-56.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 12)
510FM-06 AI 4-57.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 13)
4-58.1 AI 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-26 (Sheet 14)
510FM-06 AI 4-59.1
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-26 (Sheet 15)
4-60.1 AI 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 AH 4-61
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 1 of 15)*
4-62 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 2)*
510FM-06 AH 4-63
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 3)*
4-64 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 4)*
510FM-06 AH 4-65
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 5)*
4-66 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 6)*
510FM-06 AH 4-67
SECTION IV - PERFORMANCE MODEL 510
TAKEOFF
FAA APPROVED
U.S. Configuration
Figure 4-28 (Sheet 7)*
4-68 AH 510FM-06
MODEL 510 SECTION IV - PERFORMANCE
TAKEOFF
FAA APPROVED
Configuration U.S.
Figure 4-28 (Sheet 8)*
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Citation Mustang airplane flight manual 2(4)
