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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
ADVERSE WEATHER/ABNORMAL
ATMOSPHERIC CONDITIONS
APPENDIX E
E-62 FAA APPROVED
GIV-SP 13 September 2000
The theory that if you avoid thunderstorms you will avoid all lightning strikes or if you are
greater than 20 miles from radar-indicated precipitation, you are not susceptible to lightning
strikes are false. Airplanes have been struck by the proverbial "Bolt From The Blue" on more
than one occasion at distances up to 50 miles in clear air especially at higher altitudes.
Flying through Precipitation, Volcanic Ash, or Heavily Polluted Air can cause an airplane to
experience electrostatic discharge or triggered lightning.
The probability of a lightning strike to an airplane flying in or near a thunderstorm increases from
a minimum at the thunderstorm base to a maximum at the 36,000 to 40,000 foot level. Lightning
strikes at high altitude generally results in greater total charge transfers and damage is usually
worse for large total current transfers. The entire surface of the airplane may be susceptible to
lightning attachment even though strikes are more probable to particular areas such as the
airplane extremities (Nose, Wingtips, Tail) and composite surfaces. Electrical activity generated
by thunderstorms may exist even after the thunderstorm cell has decayed.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
FAA APPROVED 5- i
31 May 2001
TABLE OF CONTENTS
SECTION 5.1 GENERAL
INTRODUCTION.........................................................................................................5.1-1
BASIS FOR DATA.......................................................................................................5.1-2
DEFINITIONS..............................................................................................................5.1-2
FLAP POSITIONS........................................................................................................5.1-5
DEMONSTRATED CROSSWIND..............................................................................5.1-5
WET RUNWAY CONDITIONS..................................................................................5.1-5
NOISE STANDARDS..................................................................................................5.1-5
TAKEOFF WEIGHT DETERMINATION PROCEDURE .........................................5.1-6
CONVERSION CHARTS ............................................................................................5.1-7
VELOCITY CONVERSION............................................................................5.1-8
CROSSWIND COMPONENTS .......................................................................5.1-9
TEMPERATURE CONVERSION.................................................................5.1-10
AIR TEMPERATURE vs ISA CONVERSION.............................................5.1-11
DISTANCE CONVERSION ..........................................................................5.1-12
WEIGHT CONVERSION ..............................................................................5.1-13
PRESSURE CONVERSION ..........................................................................5.1-14
CABIN ALT. VS. AIRCRAFT ALT. VS. DIFFERENTIAL PRESSURE....5.1-15
POSITION ERROR ....................................................................................................5.1-16
AIRSPEED POSITION ERROR, STANDBY SYSTEM ..............................5.1-17
FLAPS 0°, SEA LEVEL TO 45,000 FT.............................................5.1-17
FLAPS 10°, SEA LEVEL TO 20,000 FT...........................................5.1-18
FLAPS 20°, SEA LEVEL TO 20,000 FT...........................................5.1-19
FLAPS 39°, SEA LEVEL TO 20,000 FT...........................................5.1-20
MACHMETER POSITION ERROR, STANDBY SYSTEM........................5.1-21
ALTITUDE POSITION ERROR, STANDBY SYSTEM..............................5.1-22
FLAPS 0°, SEA LEVEL TO 20,000 FT.............................................5.1-22
FLAPS 0°, 30,000 FT TO 45,000 FT..................................................5.1-23
FLAPS 10°, SEA LEVEL TO 20,000 FT...........................................5.1-24
FLAPS 10°, 30,000 FT........................................................................5.1-25
FLAPS 20°, SEA LEVEL TO 20,000 FT...........................................5.1-26
FLAPS 39°, GEAR DOWN, SEA LEVEL TO 20,000 FT.................5.1-27
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
PERFORMANCE
5- ii FAA APPROVED
31 May 2001
TABLE OF CONTENTS
STALL SPEEDS - IDLE POWER..............................................................................5.1-28
　
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