SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 7)*
S4-32 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 8)*
510FM-S4-02 S4-AH S4-33
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 9)*
S4-34 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 10)*
510FM-S4-02 S4-AH S4-35
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 11)*
S4-36 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 12)*
510FM-S4-02 S4-AH S4-37
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 13)*
S4-38 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 14)*
510FM-S4-02 S4-AH S4-39
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 15)*
S4-40 S4-AH 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
available distance, the airplane weight must be reduced until distance required is less than or equal
to distance available.
Figure S4-3
510FM-S4-02 S4-AI S4-25.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 1 of 15)
S4-26.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 2)
510FM-S4-02 S4-AI S4-27.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 3)
S4-28.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 4)
510FM-S4-02 S4-AI S4-29.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 5)
S4-30.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 6)
510FM-S4-02 S4-AI S4-31.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 7)
S4-32.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 8)
510FM-S4-02 S4-AI S4-33.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 9)
4-34.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 10)
510FM-S4-02 S4-AI 4-35.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 11)
S4-36.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 12)
510FM-S4-02 S4-AI S4-37.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 13)
S4-38.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 14)
510FM-S4-02 S4-AI S4-39.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 15)
S4-40.1 S4-AI 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS 15°
WET RUNWAY OVER A 15 FOOT SCREEN HEIGHT, ANTI-ICE OFF
Determine takeoff field length, V1, VR, V2 and VENR from Figure S4-6. If the runway has a gradient,
adjust V1 and takeoff field length using Figure S4-5. If the required distance is greater than the
available distance, the airplane weight must be reduced until distance required is less than or equal
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