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SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.2-9
31 May 2000 GIV-SP
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.2-10 FAA APPROVED
GIV-SP 31 May 2000
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.2-11
31 May 2000 GIV-SP
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.2-12 FAA APPROVED
GIV-SP 31 May 2000
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.2-13
31 May 2000 GIV-SP
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.2-14 FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.3-1
30 May 2002 GIV-SP
SECTION 5.3 CLIMB LIMITED PERFORMANCE
Takeoff gross weight is limited when available climb gradient is less than the minimum
allowable climb gradient. The FAR takeoff climb performance is limited by the most restrictive
of the following 3 engine-out climb requirements:
(1) A 2.4% climb gradient at 400 feet above takeoff surface with Takeoff Thrust and
takeoff flaps (10° or 20°).
(2) A 1.2% climb gradient at 1500 feet above takeoff surface with Maximum Continuous
Thrust and clean configuration.
(3) A 2.1% climb gradient at 0 feet above takeoff surface with Go-Around Thrust and
flaps 20°. (This last item is needed because the GIV does not have a fuel jettisoning
system.)
Conditions:
(1) Landing gear retracted
(2) Flaps 10° or 20°
(3) One engine inoperative
(4) Operating engine at Takeoff Thrust
(5) V2 speed
EXAMPLE: Find maximum allowable takeoff gross weight:
Given: Airport Ambient Temperature.................................................................................25°C
Airport Pressure Altitude ....................................................................................8000 ft.
Anti-Icing ................................................................................................................ OFF
Flaps ..........................................................................................................................20°
Solution: Enter the Flaps 20° / Anti-Icing Off MAXIMUM ALLOWABLE TAKEOFF GROSS
WEIGHT PERMITTED BY TAKEOFF CLIMB REQUIREMENTS chart at 25°C,
proceed right to 8000 ft., then down to determine the maximum allowable takeoff
gross weight = 70,200 pounds (31,840 kg).
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.3-2 FAA APPROVED
GIV-SP 30 May 2002

　
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