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ADVERSE WEATHER/ABNORMAL
ATMOSPHERIC CONDITIONS
APPENDIX E
FAA APPROVED E-47
13 September 2000 GIV-SP
Right Engine:
NOTE: Reduce electrical loads on APU alternator to allow APU to provide maximum airflow.
1. Utility Pump........................................................................................................................OFF
CAUTION: WITH UTILITY PUMP OFF, ONLY THE PARKING BRAKE IS AVAILABLE
TO HOLD THE AIRPLANE. THE USE OF CHOCKS IS RECOMMENDED.
2. Boost Pump............................................................................................................ONE (1) ON
3. Crossflow Valve ..............................................................................................................OPEN
4. Ram Air Switch ................................................................................................................RAM
5. Airstart Ignition.................................................................................................................... ON
For SN 1144 and subs. and earlier airplanes with ASC 151 installed.
6. HP RPM......................................16 to 22% ...............................MAX available
7. HP Fuel Cock...................................................................................................................OPEN
8. TGT..........................................................................................................................MONITOR
After Engine Stabilizes at Idle,
9. Airstart Ignition...................................................................................................................OFF
10. Utility Pump......................................................................................................................... ON
Left Engine:
1. Increase available bleed air using right engine (If Required).
CAUTION: Use only one source of air, either APU air only or crossbleed air only, to start
engine.
2. HP RPM......................................16 to 22% ................................MAX available
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
ADVERSE WEATHER/ABNORMAL
ATMOSPHERIC CONDITIONS
APPENDIX E
E-48 FAA APPROVED
GIV-SP 13 September 2000
3. Airstart Ignition ..................................................................................................................... ON
For SN 1144 and subs. and earlier airplanes with ASC 151 installed.
4. HP Fuel Cock ....................................................................................................................OPEN
5. TGT...........................................................................................................................MONITOR
After Engine Stabilizes at Idle,
6. Airstart Ignition ....................................................................................................................OFF
7. Right Engine......................................................................................................... Reduce to Idle
8. Utility Pump ...............................................................................................................NORMAL
TAXI
Ground idles may be lower than required to keep the alternators on line. It is recommended that
the APU remain running with the APU Alternator ON for all ground operations.
CAUTION: Use only one source of air, either APU air only or engine bleed air only, while
taxiing to prevent possible damage to APU.
TAKEOFF
1. Certain high elevation airports have preferential runways for takeoff and landing, i.e.,
upslope for landing and downslope for takeoff. Slope and headwind/tailwind conditions
should be given due consideration.
2. Stabilize engine power at 1.5 EPR and perform a rolling takeoff, runway length permitting.
With tailwind conditions, monitor LP RPM limits when setting final takeoff power, during
takeoff run, and during climb out. The pilot-not-flying should be briefed to monitor LP
RPM during takeoff and be ready to adjust power as necessary to avoid exceedances. The
pilot-flying should be aware that a red ENGINE EXCEEDANCE CAS message may occur
during takeoff if LP RPM exceeds 95.5%. DO NOT BE SPRING LOADED TO ABORT
THE TAKEOFF IF THIS MESSAGE OCCURS. This is especially true when using the
autothrottle.
3. If COWL and/or WING ANTI-ICE is used for takeoff, select a minimum of 1.2 EPR or
higher before selecting ANTI-ICE ON.
4. Expect slower than normal acceleration to 60 knots.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
ADVERSE WEATHER/ABNORMAL
ATMOSPHERIC CONDITIONS
APPENDIX E
FAA APPROVED E-49
13 September 2000 GIV-SP
DESCENT, APPROACH AND LANDING
1. It may be necessary to increase cabin altitude for landing.
　
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