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3-iv FAA APPROVED
11 October 2001
TABLE OF CONTENTS
SUBJECT: SECTION: PAGE:
Indicating/Recording System ..................................................... 3-18-00 ..................3-89
Display Unit Failure.................................................................. 3-18-10 ..................3-89
Symbol Generator Failure......................................................... 3-18-20 ..................3-92
Traffic and Collision Avoidance System (TCAS) Failure........ 3-18-30 ..................3-94
Enhanced Ground Proximity Warning System
(EGPWS) Failure...................................................................... 3-18-40 ..................3-94
DADC Failure........................................................................... 3-18-50 ..................3-94
Landing Gear/Landing Gear Systems ....................................... 3-19-00 ..................3-95
Landing Gear Alternate Operation............................................ 3-19-20 ..................3-95
Nosewheel Steering Failure ...................................................... 3-19-30 ..................3-98
Nutcracker System Fails To Shift To Ground
Mode At Touchdown................................................................ 3-19-40 .................3-100
Nutcracker System Fails To Shift To Air
Mode At Takeoff ...................................................................... 3-19-50 .................3-101
Landing, Stopping and Evacuation ........................................... 3-20-00 .................3-102
Planned Airplane Evacuation ................................................... 3-20-50 .................3-102
Overheat/Hot Conditions............................................................ 3-21-00 .................3-103
Under Floor Overheat ............................................................... 3-21-60 .................3-103
Pressurization/Bleed Air Systems .............................................. 3-22-00 .................3-104
Loss of Automatic Pressurization Control................................ 3-22-30 .................3-104
Pressurization System - Rate Limiting ..................................... 3-22-40 .................3-106
Bleed Air System Failure.......................................................... 3-22-50 .................3-107
Thrust Reverser System.............................................................. 3-24-00 .................3-110
Thrust Reverser Locking Procedure ......................................... 3-24-20 .................3-110
Amber Caution Messages .................................................................. ....................... 3A-1
Blue Advisory Messages..................................................................... ....................... 3B-1
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-1
13 September 2000
3-00-00: ABNORMAL PROCEDURES
3-00-10: General Guidance:
In handling abnormal situations, the following shall apply:
1. Maintain control of the airplane.
2. 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.
3-01-00: AIR CONDITIONING SYSTEM
3-01-10: Air Conditioning System Shut Down or Inoperative:
At altitude above 41,000 ft. with either Air Conditioning System OFF or inoperative, the
respective engine cowl anti-ice must be ON with Bleed Air isolation valve closed (See BLEED
AIR SYSTEM LIMITATIONS, Section 1).
3-01-20: Air Conditioning Airflow Hot or Uncontrollable:
If cool air is not produced in either AUTO or MANUAL or OFF mode, the water separator may
be frozen. With the water separator frozen, cool air can not flow through it. To determine
whether the water separator is frozen or the Air Cycle Machine (ACM) is developing a problem,
select appropriate Air Conditioning Pack switch OFF. Wait ten (10) minutes, then reselect pack
switch ON. If cool air flow is present, the water separator is most likely the problem. Select
slightly warmer temperature in effort to preclude water separator from re-freezing. If warm or
hot air flow returns, the ACM is developing a problem. Depending on flight conditions or
mission requirements, the problem pack should be managed as required. See Air Conditioning
System Shutdown or Inoperative Procedure, this Section, for bleed air requirements with the air
conditioning packs shut off.
CAUTION: DO NOT TURN BOTH PACKS OFF AT HIGH ALTITUDE.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-2 FAA APPROVED
31 May 2000
3-01-30: Left or Right Cooling Turbine Hot:
　
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