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Figure S4-2 (Sheet 6)*
510FM-S4-02 S4-AH S4-15
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 7)*
S4-16 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 8)*
510FM-S4-02 S4-AH S4-17
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 9)*
S4-18 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 10)*
510FM-S4-02 S4-AH S4-19
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 11)*
S4-20 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 12)*
510FM-S4-02 S4-AH S4-21
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 13)*
S4-22 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 14)*
510FM-S4-02 S4-AH S4-23
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 15)*
S4-24 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, WITH FLAPS UP
WET RUNWAY OVER 15 FOOT SCREEN HEIGHT, ANTI-ICE OFF
Determine takeoff field length, V1, VR, V2, and VENR from Figure S4-2. If the runway has a
gradient, adjust V1 and Takeoff Field Length using Figure S4-1. 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 S4-1
510FM-S4-02 S4-AI S4-9.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 1 of 15)
S4-10.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 2)
510FM-S4-02 S4-AI S4-11.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 3)
S4-12.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 4)
510FM-S4-02 S4-AI S4-13.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 5)
S4-14.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 6)
510FM-S4-02 S4-AI S4-15.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 7)
S4-16.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 8)
510FM-S4-02 S4-AI S4-17.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 9)
S4-18.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 10)
510FM-S4-02 S4-AI S4-19.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 11)
S4-20.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 12)
510FM-S4-02 S4-AI S4-21.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 13)
S4-22.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-2 (Sheet 14)
510FM-S4-02 S4-AI S4-23.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-2 (Sheet 15)
S4-24.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS UP
WET RUNWAY OVER A 15 FOOT SCREEN HEIGHT, ANTI-ICE ON
Determine takeoff field length, V1, VR, V2 and VENR from Figure S4-4. If the runway has a gradient,
adjust V1 and takeoff field length using Figure S4-3. If the required distance is greater than the
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Citation Mustang airplane flight manual 2(24)
