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7. Bank Angle .............................................................................. MAINTAIN TO HIGH FINAL
The bank angle should be held at 25 degrees or as necessary for turning to high final, depending
on winds.
8. Landing Gear..................................................... BLOW DOWN BEFORE TURNING FINAL
9. AUX PUMP..............................................................................................ON FOR LANDING
10. Flaps.....................................................................................................................................20°
NOTE: As airspeed is reduced on final for landing, hydraulic fluid flow will decrease and flight
controls may become less responsive. Do not use Speed Brakes if possible, as this
could hasten loss of hydraulic pressure.
11. Brakes ..........................................................................................AS NECESSARY TO STOP
12. Prepare to use Emergency Brakes if required.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-20 FAA APPROVED
31 May 2000
4-10-00: ENGINE SHUTDOWN/ARISTART/SINGLE ENGINE PROCEDURES
4-10-10: Engine Failure/Shutdown in Flight:
1. Adjust power and clean up airplane for steady flight.
NOTE: Autothrottle will disengage.
2. Engine Synchronizer...........................................................................................................OFF
3. Power Lever........................................................................................... IDLE (Failed Engine)
WARNING: VERIFY PROPER ENGINE (LEFT OR RIGHT)
4. HP Fuel Cock.........................................................................................SHUT (Failed Engine)
5. Tone Warning ............................................................................................................SILENCE
6. Fuel Boost Pumps .....................................................................................OFF (Failed Engine)
7. Airstart Ignition........................................................................................ OFF (Failed Engine)
8. Electric Master Power.............................................................................. OFF (Failed Engine)
9. Electrical Load..........................................................................................CHECK/MONITOR
NOTE: APU may be used as an alternate source of Electrical Power, if desired. See APU
IN-FLIGHT OPERATION - ALTERNATE ELECTRICAL SOURCE Checklist in
Section 3.
If an engine is shut down due to extreme vibration, consideration should be given to
pulling the Fire Handle to shut off fluids.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-21
31 May 2000
10. Bleed Air Switch...................................................................................... OFF (Failed Engine)
11. Isolation Valve.................................................................................................................OPEN
12. Utility Hydraulic Pump (Left Engine Failed) ...................................................................... ON
13. Auxiliary Hydraulic Pump (Left Engine Failed) ..............................................................ARM
14. Monitor Fuel Balance for remainder of flight.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-22 FAA APPROVED
31 May 2000
4-10-20: Airstart - Immediate:
If an engine or both engines flame out in flight and mechanical failure is not suspected,
immediate relight may be attempted at any altitude and airspeed. As RPM is decreasing, perform
the following procedure immediately:
1. Power Lever...................................................................................................................... IDLE
2. Air Start Ignition.................................................................................................................. ON
NOTE: Successful relight is indicated by RPM stabilizing at idle. Allow engine(s) to stabilize
prior to advancing power lever(s). Check that engine(s) responds normally and monitor
TGT prior to advancing power lever.
AFTER RELIGHT:
3. Airstart Ignition...................................................................................................................OFF
If engine fails to relight within twenty (20) seconds, close the high pressure fuel cock. Wait at
least one (1) minute and perform AIRSTART - NORMAL procedure in this Section.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-23
31 May 2000
4-10-30: Airstart - Normal:
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(96)
