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GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE FAA APPROVED 5.3-3 30 May 2002 GIV-SP GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE 5.3-4 FAA APPROVED GIV-SP 30 May 2002 GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE FAA APPROVED 5.3-5 30 May 2002 GIV-SP GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE 5.3-6 FAA APPROVED GIV-SP 30 May 2002 GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE FAA APPROVED 5.3-7 30 May 2002 GIV-SP GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE 5.3-8 FAA APPROVED GIV-SP 31 May 2000 THIS PAGE INTENTIONALLY LEFT BLANK. GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE FAA APPROVED 5.4-1 31 May 2000 GIV-SP SECTION 5.4 TIRE SPEED LIMITED PERFORMANCE Takeoff gross weight is limited when the liftoff speed is greater than ground speed limitation on tires (195 knots). EXAMPLE: Find maximum allowable takeoff gross weight permitted by tire speed limit: Given: Airport Ambient Temperature...............................................................................-19° C Airport Pressure Altitude .................................................................................15,000 ft. Tailwind .............................................................................................................10 knots Flaps ..........................................................................................................................20° Solution: Enter the Flaps 20° MAXIMUM ALLOWABLE TAKEOFF GROSS WEIGHT PERMITTED BY TIRE SPEED chart at -19° C, proceed right to 15,000 ft., then down, following guide lines of wind scale to determine the maximum allowable takeoff gross weight = 62,800 pounds (28,486 kg). GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE 5.4-2 FAA APPROVED GIV-SP 31 May 2000 GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE FAA APPROVED 5.4-3 31 May 2000 GIV-SP GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE 5.4-4 FAA APPROVED GIV-SP 31 May 2000 THIS PAGE INTENTIONALLY LEFT BLANK. GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 5 SPECIAL PERFORMANCE FAA APPROVED 5.5-1 31 May 2000 GIV-SP SECTION 5.5 TAKEOFF SPEEDS The takeoff decision speed, V1, must meet the following FAR criteria: 1 V1 must not exceed VR 2. V1 must not exceed Maximum Brake Energy limit speed, VMBE 3. V1 must not be less than V1MCG. The takeoff speeds charts present for V1, VR, V2 and VMBE as functions of airport temperature and altitude, gross weight, and ratio V1 / VR. To achieve the accelerate-go distance, it is necessary to initiate rotation of the airplane at the recommended airspeed. Rotation of the airplane below or above recommended airspeed will result in an undershoot or an overshoot of the V2 speed at the 35 foot obstacle height. EXAMPLE 1: Determine Takeoff Speeds V1, VR, V2 Given: Airport Ambient Temperature....................................................................................-5° C Airport Pressure Altitude ......................................................................................6,000 ft. Flaps ..............................................................................................................................20° Takeoff Gross Weight ............................................................. 63,000 pounds (28,580 kg) Runway Length ..................................................................................... 7,000 ft. (2134 m) Runway Slope ................................................................................................+1% (uphill) Stopway........................................................................................................ 200 ft. ( 61m) Clearway..................................................................................................... 500 ft. (152 m) Headwind ..............................................................................................................10 knots Anti-Skid ......................................................................................................OPERATIVE Cowl and Wing Anti-Ice .............................................................................................. ON www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 2
