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Loss of Pressurization............................................................... 4-22-10 ..................4-61
Emergency Descent Procedure ................................................. 4-22-20 ..................4-62
Smoke and Fumes........................................................................ 4-23-00 ..................4-64
Smoke and Fumes Evacuation.................................................. 4-23-10 ..................4-64
Smoke in Baggage Compartment, Aft Galley,
Lavatory or Right Hand Avionics............................................. 4-23-20 ..................4-66
Thrust Reverser System.............................................................. 4-24-00 ..................4-68
Reverse Thrust Unlock or Deploy ............................................ 4-24-10 ..................4-68
Windshields/Door Systems ......................................................... 4-25-00 ..................4-70
Windshield Failure ................................................................... 4-25-10 ..................4-70
Red Warning Messages...................................................................... ....................... 4A-1
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-iv FAA APPROVED
31 May 2000
THIS PAGE INTENTIONALLY LEFT BLANK
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-1
13 September 2000
4-00-00: EMERGENCY PROCEDURES
4-00-10: General Guidance:
In the event of any emergency the following shall apply:
1. Maintain control of the airplane.
2. Other than retracting the landing gear and silencing aural warnings, take no action until
above 400 ft. AGL.
3. Analyze the situation and take appropriate action. Resetting “popped” circuit breakers is not
recommended unless the affected system is required for continued safe flight and landing.
4. Land as soon as conditions permit.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-2 FAA APPROVED
31 May 2000
4-05-00: BRAKES SYSTEM
4-05-10: Emergency Brakes (Brake-By-Wire):
In the event of loss of Combined, Utility, and Auxiliary System pressure, the wheel brakes may
be operated by brake accumulator pressure through use of the PARK/EMERG brake handle,
which by-passes pedal control. A fully charged brake accumulator allows approximately 5 to 6
applications of the PARK/EMERG handle before the pressure is depleted.
There is a noticeable delay in pressure rise when using the parking brake handle to meter
pressure. Grasp the handle with fingertips only and rest the thumb near the base of the speed
brake handle slot. Raise the handle carefully in 1/4 inch increments to avoid excessive pressure.
CAUTION: ANTI-SKID PROTECTION IS NOT AVAILABLE WHEN USING THE
EMERGENCY BRAKE SYSTEM. USE OF THE EMERGENCY BRAKE
SYSTEM WHILE THE AIRPLANE IS MOVING IS STRICTLY AN
EMERGENCY PROCEDURE. THE EMERGENCY BRAKE PRESSURE CAN
BE METERED. CAUTION SHOULD BE USED NOT TO EXTEND HANDLE
BEYOND THE POSITION WHERE BRAKING IS FIRST FELT [1/4 TO 1/2
INCH (O.635 TO 1.27 CM)]. AS AIRPLANE DECELERATES,
REPOSITIONING (METERING) OF HANDLE (EASING IN) MIGHT BE
NECESSARY TO PREVENT SUDDEN STOPPING OR TIRE SKIDDING.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-3
31 May 2000
4-05-20: Emergency Brakes (HMAB):
For airplanes SN 1183, SN 1214 and subs. with the Hydromechanical Analog Brake (HMAB)
System incorporated:
Emergency braking is available using the parking brake handle to meter accumulator pressure
directly to the brakes.
Anti-skid protection is bypassed and pressure must be limited to 300 psi to avoid locked wheels
and blown tires.
It is normal for deceleration to increase during the stop even though applied pressure is held
constant. Reduce pressure as required to maintain constant deceleration.
There is a noticeable delay in pressure rise when using the parking brake handle to meter
pressure. Grasp the handle with fingertips only and rest the thumb near the base of the speed
brake handle slot. Raise the handle carefully in 1/4 inch increments to avoid excessive pressure.
CAUTION: ANTI-SKID PROTECTION IS NOT AVAILABLE WHEN USING THE
EMERGENCY BRAKE SYSTEM. USE OF THE EMERGENCY BRAKE
SYSTEM WHILE THE AIRPLANE IS MOVING IS STRICTLY AN
EMERGENCY PROCEDURE. THE EMERGENCY BRAKE PRESSURE CAN
BE METERED. CAUTION SHOULD BE USED NOT TO EXTEND HANDLE
BEYOND THE POSITION WHERE BRAKING IS FIRST FELT [1/4 TO 1/2
INCH (O.635 TO 1.27 CM)]. AS AIRPLANE DECELERATES,
　
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