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to maintain 300 psi.
CAUTION: IT IS NORMAL FOR DECELERATION TO INCREASE AS
THE STOP PROGRESSES. IT IS EXTREMELY IMPORTANT TO
MAINTAIN 300 PSI TO AVOID LOCKED WHEELS AND BLOWN TIRES.
THERE WILL BE A SIGNIFICANT INCREASE IN LANDING DISTANCE
WITH ANTI-SKID INOPERATIVE.
NOTE: Brake pedal position in relation to brake pressure can be
observed and practiced airborne with the anti-skid system selected OFF,
and the landing gear up or down.
NOTE: An increase in landing distance will result if landing rollout is
made with anti-skid completely inoperative. For landing distances with
anti-skid inoperative, refer to Landing Field Length, Anti-Skid Inoperative
charts in Performance section of GIV AFM. Use of reverse thrust reduces
landing distances.
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EC - 1
Engines Index
Engine Failure During Takeoff Below V1 Speed ..................... EC-2
Engine Failure During Takeoff Above V1 Speed ..................... EC-2
Dual Engine Flameout ............................................................... EC-3
Dual Engine Out Speeds For Maximum Range....................... EC-5
Dual Engine Out Approach and Landing................................. EC-5
Engine Failure / Shutdown In Flight......................................... EC-6
Engine Out Driftdown - ISA....................................................... EC-7
Airstart - Immediate ................................................................... EC-9
Airstart - Normal......................................................................... EC-9
One (1) Engine Inoperative Landing Procedure.................... EC-10
One (1) Engine Inoperative Go-Around Procedure............... EC-11
Reverse Thrust Unlock or Deploy .......................................... EC-11
Thrust Reverser Locking Procedure .......................................... EC-13
Engine Synchronizer Failure ...................................................... EC-14
Approach Idle System Failure .................................................... EC-15
Engine Vibration......................................................................... EC-15
Ice Shedding Procedure............................................................. EC-16
Engine Failure To Start .............................................................. EC-16
Start Valve Failure...................................................................... EC-17
Start Valve Open (SVO) Indication In Flight............................... EC-18
Hot Start ..................................................................................... EC-18
Continuous (Airstart) Ignition Limitations ................................... EC-18
Airstart Envelope........................................................................ EC-19
Related Topics In QRH
Shutdown ..................................................................................... NF-1
Engine Cranking Cycle.................................................................NG-1
Engine Start - Battery Power Only ...............................................NG-2
Single Engine Taxi .......................................................................NG-3
Landing Planning Data...............................................PC-1 thru PC-14
APU Inflight Operation - Alternate Electrical Source...................EA-27
APU Inflight Operation - ELWS (Loadmeter) /
ASC 420 Procedures ...............................................................EA-29
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EC - 2 May 30/02
Engine Failure During Takeoff Below V1 Speed
AFM 4-09-20
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, Page NF-1) .......
.....................................................................................COMPLETE
END
Engine Failure During Takeoff Above V1 Speed
AFM 4-09-30
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.
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湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 3(25)
