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to distance available.
Figure S4-5*
510FM-S4-01 S4-AA S4-41
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 1 of 15)*
S4-42 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 2)*
510FM-S4-01 S4-AA S4-43
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 3)*
S4-44 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 4)*
510FM-S4-01 S4-AA S4-45
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 5)*
S4-46 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 6)*
510FM-S4-01 S4-AA S4-47
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 7)*
S4-48 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 8)*
510FM-S4-01 S4-AA S4-49
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 9)*
S4-50 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 10)*
510FM-S4-01 S4-AA S4-51
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 11)*
S4-52 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 12)*
510FM-S4-01 S4-AA S4-53
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-6 (Sheet 13)*
S4-54 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-6 (Sheet 14)*
510FM-S4-01 S4-AA S4-55
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration S4-AA
Figure S4-6 (Sheet 15)*
S4-56 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS 15°
WET RUNWAY OVER A 35 FOOT SCREEN HEIGHT, ANTI-ICE ON
Determine takeoff field length, V1, VR, V2 and VENR from Figure S4-8. If the runway has a gradient,
adjust V1 and takeoff field length using Figure S4-7. 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 S4-7*
510FM-S4-01 S4-AA S4-57
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration S4-AA
Figure S4-8 (Sheet 1 of 15)*
S4-58 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 2)*
510FM-S4-01 S4-AA S4-59
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 3)*
S4-60 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 4)*
510FM-S4-01 S4-AA S4-61
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 5)*
S4-62 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 6)*
510FM-S4-01 S4-AA S4-63
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 7)*
S4-64 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 8)*
510FM-S4-01 S4-AA S4-65
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 9)*
S4-66 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-8 (Sheet 10)*
510FM-S4-01 S4-AA S4-67
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-8 (Sheet 11)*
S4-68 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
　
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