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NOTE: Small rudder doublets for the purposes of flight test of yaw damper effectiveness and
response are allowed.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-i
13 September 2000
TABLE OF CONTENTS
SUBJECT: SECTION: PAGE:
Abnormal Procedures ................................................................. 3-00-00 ...................3-1
General Guidance ..................................................................... 3-00-10 ...................3-1
Air Conditioning System............................................................. 3-01-00 ...................3-1
Air Conditioning System Shut Down Or Inoperative............... 3-01-10 ...................3-1
Air Conditioning System Airflow Hot Or Uncontrollable ....... 3-01-20 ...................3-1
Left or Right Cooling Turbine Hot ........................................... 3-01-30 ...................3-2
Anti-Skid System ......................................................................... 3-02-00 ...................3-4
Anti-Skid Failure (Brake-By-Wire).......................................... 3-02-10 ...................3-4
Anti-Skid Off Braking (Brake-By-Wire)
(SN 1000 Thru 1213 Without ASC 190/266)........................... 3-02-20 ...................3-6
Anti-Skid Off Braking (Brake-By-Wire)
(SN 1000 Thru 1213 With ASC 190/266)................................ 3-02-30 ...................3-8
Anti-Skid Failure (HMAB)....................................................... 3-02-40 ..................3-10
Anti-Skid Off Braking (HMAB)............................................... 3-02-50 ..................3-11
Auto Flight System ...................................................................... 3-03-00 ..................3-13
Autopilot Malfunction .............................................................. 3-03-10 ..................3-13
Autothrottle Malfunction.......................................................... 3-03-20 ..................3-14
AFGCS Failure ......................................................................... 3-03-30 ..................3-15
Mach Trim Compensation Failure............................................ 3-03-40 ..................3-16
Yaw Damper Failure................................................................. 3-03-50 ..................3-17
Auxiliary Power System.............................................................. 3-04-00 ..................3-18
APU Starting On External DC Power ...................................... 3-04-10 ..................3-18
APU Inflight Operation: Alternate Electrical Source .............. 3-04-20 ..................3-21
APU Inflight Operation: Alternate Electrical
Source - ELWS (Loadmeter) Procedure ................................... 3-04-30 ..................3-23
APU Alternator Failure............................................................. 3-04-40 ..................3-25
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-ii FAA APPROVED
13 September 2000
TABLE OF CONTENTS
SUBJECT: SECTION: PAGE:
Brakes System.............................................................................. 3-05-00 ..................3-26
Wheel Brake Failure ................................................................. 3-05-30 ..................3-26
Brake Confidence Check - Inflight (Brake-By-Wire)............... 3-05-40 ..................3-27
Uncommanded Applied Brake Pressure - Inflight
(Brake-By-Wire) ....................................................................... 3-05-50 ..................3-28
Landing With Applied Brake Pressure Indicated
(Brake-By-Wire) ....................................................................... 3-05-60 ..................3-30
Uncommanded Brake Pressure During Landing
Rollout (Brake-By-Wire) .......................................................... 3-05-70 ..................3-31
Auxiliary Braking (HMAB)...................................................... 3-05-80 ..................3-32
Brakes System Messages............................................................. 3-06-00 ..................3-33
Brake Fail Message (Brake-By-Wire) ...................................... 3-06-10 ..................3-33
Brake Fail Message (HMAB) ................................................... 3-06-20 ..................3-34
Brake Maintenance Required Message (HMAB) ..................... 3-06-30 ..................3-36
Brake Pedal Message (Brake-By-Wire).................................... 3-06-40 ..................3-37
Multiple Brake Failure Message (Brake-By-Wire) .................. 3-06-50 ..................3-38
BTMS OVHT Light On Or Brake OVHT Message ................. 3-06-60 ..................3-40
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(48)
