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Electrical Power System.............................................................. 3-07-00 ..................3-43
Alternator/Converter Failure - Single ....................................... 3-07-40 ..................3-43
Electrical Load Warning System (ELWS)................................ 3-07-50 ..................3-45
Flight With One Electrical System Inoperative - Secondary
Failures Using ELWS Procedures or With ASC 420
And SN 1430 and Subs............................................................. 3-07-60 ..................3-46
Figure 3-1: APU Operating Envelope ............................................ ........................3-48
Figure 3-2: APU Alternator Electrical Load Envelope................... ........................3-49
Figure 3-3: ELWS/ASC 420 APU Operating Envelope................. ........................3-50
Figure 3-4: ELWS/ASC 420 APU Alternator
Electrical Load Envelope................................................................. ........................3-51
Bus Fault - AC Or DC Reset Light On..................................... 3-07-70 ..................3-52
Battery or Battery Charger Failure............................................ 3-07-80 ..................3-62
Essential DC Bus On Battery Power ........................................ 3-07-90 ..................3-63
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-iii
11 October 2002
TABLE OF CONTENTS
SUBJECT: SECTION: PAGE:
Engine Control System................................................................ 3-08-00 ..................3-65
Engine Synchronizer Failure .................................................... 3-08-10 ..................3-65
Approach Idle System Failure .................................................. 3-08-20 ..................3-66
Engine Vibration....................................................................... 3-08-30 ..................3-67
Ice Shedding Procedures........................................................... 3-08-40 ..................3-67
Engine Starting System............................................................... 3-11-00 ..................3-68
Engine Failure To Start............................................................. 3-11-10 ..................3-68
Start Valve Failure.................................................................... 3-11-20 ..................3-70
Start Valve Open (SVO) Indication - Inflight........................... 3-11-30 ..................3-71
Hot Start.................................................................................... 3-11-40 ..................3-72
Fire Detection System.................................................................. 3-13-00 ..................3-73
Fire Detection System Fault ..................................................... 3-13-20 ..................3-73
Flaps System................................................................................. 3-14-00 ..................3-74
Failure of Stabilizer/Flap Interconnect ..................................... 3-14-10 ..................3-74
Wing Flaps - Alternate Operation............................................. 3-14-20 ..................3-75
Partial Flaps Landing................................................................ 3-14-30 ..................3-77
Undesired Flaps Movement...................................................... 3-14-40 ..................3-78
Flight Controls System................................................................ 3-15-00 ..................3-79
Runway Electric Elevator Trim ................................................ 3-15-60 ..................3-79
Frozen Pitch Trim..................................................................... 3-15-70 ..................3-80
Fuel System .................................................................................. 3-16-00 ..................3-82
Fuel Boost Pump Failure .......................................................... 3-16-20 ..................3-82
Failure of Two Boost Pumps on One Side ............................... 3-16-30 ..................3-83
Hydraulic System......................................................................... 3-17-00 ..................3-84
Utility Hydraulic Pump............................................................. 3-17-20 ..................3-84
Combined Hydraulic System Failure........................................ 3-17-30 ..................3-85
Flight Hydraulic System Failure ............................................... 3-17-40 ..................3-87
Landing With Standby Electrical Power System Operating..... 3-17-50 ..................3-88
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
　
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