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PERFORMANCE
FAA APPROVED 5.1-11
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-13
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-15
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
16
POSITION ERROR
For the Electronic Flight Instrument System (EFIS) Primary-Flight-Display (PFD), displayed
airspeed is equal to calibrated airspeed, displayed Mach number is equal to true Mach number,
and displayed altitude is equal to true altitude.
Charts for position error are provided for Standby pitot-static instruments only. These charts
permit conversion from Indicated Airspeed to Calibrated Airspeed, and from Indicated Mach
Number to True Mach Number directly. To convert Indicated Altitude to True Altitude, obtain
the altitude position error correction and add this value to the indicated altitude, i.e. HT = HI +
•Hpec where:
HT, TRUE ALTITUDE, is the Altimeter reading corrected for static source position error.
HI, INDICATED ALTITUDE, is the Altimeter reading uncorrected for static source position
error.
•Hpec is altitude position error correction from the appropriate chart.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-17
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
18
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
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PERFORMANCE
FAA APPROVED 5.1-19
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
20
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-21
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
22
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-23
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
24
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-25
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
26
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-27
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
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STALL SPEEDS - IDLE POWER
The variation of stalling speed with weight, altitude, and flap position is shown. The effect of
full extension of the speed brakes is noted on each chart.
EXAMPLE:
Flaps ......................................................................................................................................20°
Pressure Altitude .............................................................................................................5000 ft.
Gross Weight....................................................................................60,000 Pounds (27,216 kg)
Stalling Speed..........................................................................................................113.5 KCAS
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-29
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
30
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.1-31
31 May 2001
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5.1- FAA APPROVED
31 May 2001
32
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5.2-1
31 May 2001
SECTION 5.2 FIELD LENGTH LIMITED PERFORMANCE
　
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