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(ABEX) Generator is not possible with a windmilling engine.
CAUTION: MANEUVERS SHOULD BE LIMITED TO MINIMUM BANK AND PITCH
ANGLES NECESSARY SINCE HYDRAULIC BOOST WILL BE LOST AS
ENGINE RPM DECAYS.
CAUTION: FOR AIRPLANES SN 1000 THRU 1249 WITHOUT ASC 304: THE DUTY
CYCLE TIME FOR CONTINUOUS (AIRSTART) IGNITION WITHOUT ASC
304 IS FIVE (5) MINUTES ON AND THIRTY (30) MINUTES OFF FOR
COOLING THERE IS NO LIMITATION ON THE IGNITION WHEN USED IN
A THIRTY (30) SECONDS ON, THIRTY (30) SECONDS OFF CYCLE.
FOR AIRPLANES SN 1250 AND SUBS AND SN 1000 THRU 1249 WITH
ASC 304: THERE IS NO DUTY CYCLE TIME LIMITATION FOR
CONTINUOUS (AIRSTART) IGNITION WITH ASC 304.
CAUTION: ENGINE DAMAGE MAY RESULT IF RPM IS NOT ALLOWED TO
STABILIZE AT IDLE BEFORE ADVANCING POWER LEVERS.
If engine(s) DO NOT relight, continue descent to the Airstart envelope (Sea Level to 25,000 ft.
and 200 KCAS to 324 KCAS). Proceed to the nearest suitable landing site.
Refer to Dual Engine Flameout Procedure, Emergency Procedures Section 4.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
ADVERSE WEATHER/ABNORMAL
ATMOSPHERIC CONDITIONS
APPENDIX E
FAA APPROVED E-61
11 October 2002
LIGHTNING STRIKE
If both engines flameout, an immediate relight is recommended. As RPM is decreasing, perform
the following procedures immediately:
1. Power Levers..................................................................................................................... IDLE
2. Airstart Ignition.................................................................................................................... ON
3. Altitude/Airspeed............................................................. Descend at VMO/MMO to 25,000 feet
then slow to 210 KCAS.
NOTE: Use of Speed brakes is not recommended. Use of the Standby Electrical System
(ABEX) Generator is not possible with a windmilling engine.
CAUTION: MANEUVERS SHOULD BE LIMITED TO MINIMUM BANK AND PITCH
ANGLES NECESSARY SINCE HYDRAULIC BOOST WILL BE LOST AS
ENGINE RPM DECAYS.
CAUTION: FOR AIRPLANES SN 1000 THRU 1249 WITHOUT ASC 304: THE DUTY
CYCLE TIME FOR CONTINUOUS (AIRSTART) IGNITION WITHOUT ASC
304 IS FIVE (5) MINUTES ON AND THIRTY (30) MINUTES OFF FOR
COOLING THERE IS NO LIMITATION ON THE IGNITION WHEN USED IN
A THIRTY (30) SECONDS ON, THIRTY (30) SECONDS OFF CYCLE.
FOR AIRPLANES SN 1250 AND SUBS AND SN 1000 THRU 1249 WITH
ASC 304: THERE IS NO DUTY CYCLE TIME LIMITATION FOR
CONTINUOUS (AIRSTART) IGNITION WITH ASC 304.
CAUTION: ENGINE DAMAGE MAY RESULT IF RPM IS NOT ALLOWED TO
STABILIZE AT IDLE BEFORE ADVANCING POWER LEVERS.
If engine(s) DO NOT relight, continue descent to the Airstart envelope (Sea Level to 25,000 ft.
and 200 KCAS to 324 KCAS). Proceed to the nearest suitable landing site.
Refer to Dual Engine Flameout Procedure, EMERGENCY PROCEDURES, Section 4.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
ADVERSE WEATHER/ABNORMAL
ATMOSPHERIC CONDITIONS
APPENDIX E
E-62 FAA APPROVED
31 May 2001
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 2(165)
