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the approach at 20° flaps at VREF 20° +10 kts. See Performance Section for landing
distance in the flaps 20° configuration.
4. Airspeed ..........................................................................................................VREF 39° FLAPS
AFTER LANDING
5. Operating Engine Thrust Reverser...................................................................AS REQUIRED
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-27
31 May 2000
4-10-50: One (1) Engine Inoperative Go-Around Procedure:
1. Power Lever...............................................................Go-Around Power On Operating Engine
2. Flaps.....................................................................................................................................20°
3. Airspeed.......................................................................................VREF (for 20° flaps) +5 knots
4. Landing Gear ........................................ RETRACT when Positive Rate of Climb is Attained
5. Flaps................................................................................UP When VREF (20° flaps) +20 knots
(Maintain speed for adequate stall margin)
6. Power ...........................................................................MAXIMUM CONTINUOUS POWER
NOTE: Final Segment Climb performance is based on setting Maximum Continuous Power on
operating engine.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-28 FAA APPROVED
31 May 2000
4-12-00: FIRE: ENGINE/APU/ELECTRICAL/AIRCRAFT
4-12-10: Engine Fire:
The important action for controlling an engine fire is to shut the affected engine down and
shutoff the combustible fluids as quickly as possible.
For an engine fire warning (Red ENG FIRE LOOP ALRT with warning tone, accompanied by
Fire Handle Red Lights ON, and lights in the associated HP Fuel Cock), proceed as follows:
1. Warning Tone ............................................................................................................SILENCE
2. Power Lever...................................................................................................................... IDLE
NOTE: Verify proper engine (Left or Right).
If the fire warning light extinguishes with the power lever at idle, test fire warning system. If
system tests satisfactory and other engine parameters are normal, there is no need to shut down
the engine. Select engine bleed air OFF on affected engine. Open isolation valve. Maintain FL
410 or below.
If the fire warning light remains illuminated with the power lever at idle, proceed to Step 3.
3. Corresponding HP FUEL COCK ....................................................................................SHUT
4. Fire Handle ...................................................................................................................... PULL
5. Fire Extinguisher ...........................................................DISCH 1, (Turn to Extreme Position)
If the fire warnings extinguish, test the associated fire warning system. If fire warning messages
test satisfactorily, complete the ENGINE FAILURE/ SHUTDOWN Checklist.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-29
31 May 2000
If the fire warning messages do not test satisfactorily or if the fire warning lights remain
illuminated for 30 seconds after firing the first fire extinguisher, proceed as follows:
6. Fire Extinguisher ...........................................................DISCH 2, (Turn to Extreme Position)
7. ENGINE FAILURE/SHUTDOWN Checklist......................................................COMPLETE
WARNING: ENGINE MUST NOT BE RESTARTED AFTER A FIRE WARNING;
THE FIRE HANDLE MUST NOT BE PUSHED IN.
CAUTION: ABOVE PROCEDURE MUST NOT BE USED FOR IN-FLIGHT TRAINING;
SHUTTING DOWN AN ENGINE BY MEANS OF THE FIRE HANDLE MAY
LEAD TO ENGINE COMPONENT DAMAGE AND VIBRATION.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-30 FAA APPROVED
31 May 2000
4-12-20: Engine Fire On Ground:
1. Stop the airplane; Parking Brake ........................................................................................SET
2. Power Lever...................................................................................................................... IDLE
3. HP Fuel Cock...................................................................................................................SHUT
4. Fire Handle ...................................................................................................................... PULL
　
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