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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-AH S4-25
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 1 of 15)*
S4-26 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 2)*
510FM-S4-02 S4-AH S4-27
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 3)*
S4-28 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 4)*
510FM-S4-02 S4-AH S4-29
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
Figure S4-4 (Sheet 5)*
S4-30 S4-AH 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
Figure S4-4 (Sheet 6)*

　
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