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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 www.aero.cn 航空翻譯 www.aviation.cn 本文鏈接地址：Citation Mustang airplane flight manual 3
