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THE AFFECTED REVERSER. DAMAGE CAN
OCCUR TO AN ACTUATOR’S PRIMARY LOCK IF
IT IS UNLOCKED WITHOUT MAINTAINING STOW
SIDE PRESSURE ABOVE 1200 PSI. THE
ACTUATOR COULD BE DAMAGED REQUIRING
REPLACEMENT AND/OR LOCK DOWN
PROCEDURES MORE RESTRICTIVE THAN THE
INITIAL FAILURE WOULD DICTATE.
SMOKE DETECT SMOKE DETECT Smoke in area
annunciated by
illuminated indication.
Refer to Emergency
Procedures Section 4, for
area in which smoke is
detected.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 5
SPECIAL
PERFORMANCE
FAA APPROVED 5- i
31 May 2000 GIV-SP
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 UP (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 UP (0°), SEA LEVEL TO 20,000 FT ....................................5.1-22
FLAPS UP (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
SPECIAL
PERFORMANCE
5- ii FAA APPROVED
GIV-SP 31 May 2000
TABLE OF CONTENTS
STALL SPEEDS - IDLE POWER..............................................................................5.1-28
FLAPS UP (0°) ...............................................................................................5.1-29
FLAPS 10° ......................................................................................................5.1-30
FLAPS 20° ......................................................................................................5.1-31
FLAPS 39° ......................................................................................................5.1-32
SECTION 5.2 FIELD LENGTH LIMITED PERFORMANCE...............................................5.2-1
MAXIMUM ALLOWABLE TAKEOFF GROSS WEIGHT PERMITTED BY
FIELD LENGTH REQUIREMENTS...........................................................................5.2-6
FLAPS 20° ........................................................................................................5.2-6
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(113)
