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2. Extreme engine vibration is felt in airframe.
NOTE: EVM indications alone should not be used as criteria for engine shutdown. If EVM
exceeds 0.60 LP and/or 0.60 HP, retard power lever to achieve vibration below this
value. If vibration is accompanied by other failure indication, shut down engine. In
icing conditions, vibrations may exceed ALERT LEVEL without other abnormal
indications and are considered normal.
3. Excessive or uncontrollable power loss.
4. Sudden rise or drop in oil pressure beyond limits.
5. Sustained high engine oil temperature above limits.
6. Sudden uncontrollable rise in TGT beyond limits.
7. Any other condition that indicates the advisability of engine shutdown.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-14 FAA APPROVED
31 May 2000
4-09-20: Engine Failure During Takeoff Below V1 Speed:
1. Power Levers .................................................................................................................... IDLE
NOTE: Autothrottle will disconnect.
2. Maximum Anti-Skid Braking..........................................................................AS REQUIRED
3. Speed Brakes..................................................................................DEPLOY IMMEDIATELY
NOTE: Ground spoilers should deploy automatically when the power levers are closed during
an aborted takeoff. Speed brake deployment is a required backup procedure.
4. Thrust Reversers ..............................................................................................AS REQUIRED
5. AFTER LANDING Checklist (when clear of runway) ........................................COMPLETE
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-15
31 May 2000
4-09-30: Engine Failure During Takeoff Above V1 Speed:
1. Yaw toward dead engine can be expected. Use corrective directional control as necessary.
NOTE: Autothrottle will disconnect.
2. Rotate airplane at VR speed and accelerate to V2 after lift off.
NOTE: Additional rudder input will be required when nose wheel lifts off.
3. Gear UP when positive rate of climb is established.
4. Maintain V2 speed to 1500 ft. AGL.
NOTE: If engine failure should occur after passing V2 on takeoff, it is recommended that the
speed at the time of engine failure (up to V2+10 knots) be maintained. A speed of
V2+10 knots in single-engine takeoff configuration will produce the maximum climb
gradient available.
5. Flaps............................. UP When VFS is Attained (Maintain speed for adequate stall margin)
6. Power ...........................................................................MAXIMUM CONTINUOUS POWER
7. ENGINE FAILURE/SHUTDOWN IN-FLIGHT CHECKLIST...........................COMPLETE
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-16 FAA APPROVED
11 October 2002
4-09-40: Dual Engine Flameout:
If flameout is the result of volcanic ash encounter, an immediate relight is not recommended.
Reverse course to clear ash cloud and proceed to Step 3.
1. Power Levers .................................................................................................................... IDLE
2. Airstart Ignition.................................................................................................................... ON
3. Airspeed......................................................................... DESCEND at VMO/MMO to 25,000 ft.
then slow to 210 KCAS (not to exceed Mach limitations).
If engines fail to relight,
4. Oxygen Masks/Regulators ................................................................ DON/100% (If Required)
5. Passenger Oxygen Masks .....................................................................DEPLOY (If Required)
6. Power Levers .................................................................................................................... IDLE
7. HP Fuel Cocks .................................................................................................................SHUT
If below 28,000 ft. proceed to Step 15.
8. Airstart Ignition...................................................................................................................OFF
9. Battery Switches 1 and 2.........................................................................................ON (Verify)
10. Essential AC/DC Buses ......................................................................... E INV/BATT (Verify)
11. Electric Master Power Switches ........................................................................ OFF (L and R)
12. Crossflow/Boost Pumps.......................................................................... OPEN/One Main-ON
　
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