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1. Convert Knots to Miles-Per-Hour, or Miles-Per-Hour to Knots.
2. Compute crosswind component and headwind or tailwind component, given wind speed
and angle from flight path.
3. Convert degrees Fahrenheit to degrees Celsius, or degrees Celsius to degrees Fahrenheit.
4. Compute deviation from International Standard Atmosphere (ISA) given air temperature
and altitude, or compute air temperature given altitude and deviation from ISA.
5. Convert Feet to Meters, or Meters to Feet.
6. Convert Pounds to Kilograms, or Kilograms to Pounds.
7. Convert inches of mercury to Millibars, or Millibars to inches of mercury.
8. Convert Cabin Altitude to Airplane Altitude Differential Pressure, or Airplane Altitude to
Cabin Altitude Differential Pressure.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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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
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
20
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
23
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
24
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5.1-
31 May 2000 GIV-SP
25
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
5.1- FAA APPROVED
GIV-SP 31 May 2000
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