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ALTITUDE/TEMPERATURE OPERATING ENVELOPE.
NOTE: Inadvertent encounters with atmospheric conditions where the SAT is colder than -70°C
can occur. To not exceed structure and equipment design temperature limits, the
following minimum Mach schedule shall be maintained until the airplane can return to
operations within the envelope.
SAT - °C -70 -72 -74 -76 -78 -80
Min - M .67 .71 .76 .80 .84 .87
1-03-30: Maximum Operating Altitude:
Maximum Operating Altitude is 45,000 ft.
1-03-40: Maximum Landing Gear Extended Operating Altitude:
Maximum Operating Altitude for extending landing gear or flying with landing gear extended is
20,000 ft. MSL.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-6 FAA APPROVED
31 May 2000
Figure 1-1: Altitude/Temperature Operating Envelope
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-7
31 May 2000
1-03-50: Maximum Landing Flaps Extended Operating Altitude:
Maximum operating altitude for extending landing flaps (39°) or flying with landing flaps
extended is 20,000 ft. MSL.
1-03-60: Airspeed Limitations:
A. MAXIMUM OPERATING LIMIT SPEED (VMO/MMO)
Maximum Operating Limit Speed shall not be deliberately exceeded in any regime of flight
(climb, cruise, or descent). See figure titled ALTITUDE-MACH FLIGHT ENVELOPE.
B. MANEUVERING SPEED (VA)
Maximum deflection of flight controls should not be used at speeds in excess of 170 KCAS.
Maximum deflection of flight controls should not be used at speeds in excess of 206 KCAS (for
airplanes SN 1214 and subs. and airplanes SN 1000 thru 1213 with ASC 190.)
C. TURBULENCE PENETRATION SPEED
Maximum Turbulence Penetration Speeds are 270 KCAS/0.75 MT.
D. MACH TRIM/ELECTRIC ELEVATOR TRIM INOPERATIVE
With both Mach Trim Compensators inoperative or electric elevator trim inoperative the
maximum operating limit speed is 0.75 MT.
E. YAW DAMPER INOPERATIVE
With Yaw Damper inoperative, maintain at least 220 KCAS above 18,000 ft.
F. FLAPS EXTENDED SPEED (VFE/MFE)
Takeoff 10° flaps - 250 KCAS/ 0.60 MT
Takeoff/approach 20° flaps - 220 KCAS/0.60 MT
Landing 39° flaps - 170 KCAS/0.60 MT
39° flaps - 180 KCAS/0.60 MT (for airplanes SN 1214 and
subs. and airplanes SN 1000 thru 1213 with ASC 190.)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-8 FAA APPROVED
31 May 2000
G. LANDING GEAR OPERATING SPEED (VLO/MLO)
Do not lower or raise landing gear at speeds in excess of 225 KCAS/0.70 MT. Do not lower
landing gear utilizing alternate system at speeds in excess of 175 KCAS.
H. LANDING GEAR EXTENDED SPEED (VLE/MLE)
Do not fly at speeds in excess of 250 KCAS/0.70 MT with landing gear extended (gear doors
open or closed).
I. MINIMUM CONTROL SPEED (VMC)
Minimum Control Speed, Air is 104 KCAS. Minimum Control Speed, Ground is 111 KCAS.
J. WINDSHIELD WIPER OPERATION SPEED
Do not operate windshield wipers at speeds in excess of 200 KCAS.
K. MAXIMUM TIRE SPEED
AIRPLANE
SERIAL NUMBER
CONFIGURATION NOSE MAIN OVERALL
LIMIT
1000 - 1213 W/O ASC 190/266 182 KTS/210 MPH 182 KTS/210 MPH 182 KTS/210 MPH
1000 - 1213 With ASC 266 182 KTS/210 MPH 195 KTS/225 MPH 182 KTS/210 MPH
1000 - 1213 With ASC 190 195 KTS/225 MPH 195 KTS/225 MPH 195 KTS/225 MPH
1214 - Sub Production 195 KTS/225 MPH 195 KTS/225 MPH 195 KTS/225 MPH
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-9
31 May 2000
Figure 1-2: Altitude - Mach Flight Envelope
(SN 1000 and subsequent)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-10 FAA APPROVED
31 May 2000
Figure 1-3: Altitude - Mach Flight Envelope
(SN 1000 - 1214 with ASC 61)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-11
13 September 2000
1-03-70: Flight Load Acceleration Limits:
A. FLAPS UP -1.0 to 2.5 G for all weights up to maximum takeoff
B. FLAPS DOWN 0 to 2.0 G for all weights up to maximum landing
1-03-80: Weight Limitations:
AIRPLANE
SERIAL NUMBER
MAXIMUM
ZERO FUEL
MAXIMUM
RAMP
MAXIMUM
TAKEOFF (1)
MAXIMUM
LANDING (2)
1000 THRU 1213 46,500 lb
(21,092 kg)
73,600 lb
(33,385 kg)
73,200 lb
(33,204 kg)
58,500 lb
(26,536 kg)
1000 THRU 1213
ASC 61
49,000 lb
(22,226 kg)
73,600 lb
(33,385 kg)
73,200 lb
(33,204 kg)
58,500 lb
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(17)
