曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EE - 3
General Guidance AFM 4-15-10
CAUTION: DO NOT PULL THE FLIGHT POWER SHUTOFF HANDLE
WITH THE SPEED BRAKES EXTENDED, AS ASYMMETRICAL SPOILER
BLOWDOWN MAY CAUSE AIRPLANE ROLL. SHOULD THE FLIGHT
POWER SHUTOFF HANDLE INADVERTENTLY BE PULLED WITH SPEED
BRAKES EXTENDED, IMMEDIATELY MOVE THE SPEED BRAKE HANDLE
TO THE FULL RETRACTED POSITION.
END
Flight Control Runaway To Hardover Position
AFM 4-15-20
Rudder Control (Yaw):
1. Flight Power Shutoff Handle....................................................PULL
Aileron Control (Roll):
2. Check GND SPOILER message. If extinguished:
Flight Power Shutoff Handle....................................................PULL
Elevator Control (Pitch):
3. Verify runaway electric trim or stall barrier is not the problem, then:
Flight Power Shutoff Handle...................................................PULL
END
Immovable Flight Controls AFM 4-15-30
Rudder Control (Yaw):
1. Flight Power Shutoff Handle.............................................. DO NOT
PULL UNLESS COUPLED WITH SINGLE ENGINE EMERGENCY
Aileron Control (Roll):
2. Flight Power Shutoff Handle....................................................PULL
Elevator Control (Pitch):
3. Flight Power Shutoff Handle....................................................PULL
NOTE: Use only lateral and longitudinal trim after pulling Flight Power
Shutoff Handle. Disengage yaw damper. Return directional trim to the
neutral position prior to restoring hydraulic boost to flight control. If control
is not regained in manual mode, return hydraulic boost to flight controls.
NOTE: If yaw damper disengages as result of pulling Flight Power
Shutoff Handle, do not attempt to re-engage it until hydraulic pressure has
been restored to flight controls.
END
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EE - 4 May 30/02
Stall Barrier Malfunction AFM 4-15-40
In the event of unwanted stall barrier actuation:
1. Autopilot Disengage Button..............................PRESS AND HOLD
2. Stall Barrier Switch....................................................................OFF
3. Autopilot Disengage Button............................................. RELEASE
4. Determine failed stall barrier system and disable by pulling the
appropriate STALL WARN CMPTR circuit breaker (#1: CPO, A-11;
#2: CPO, B-11.)
5. Stall Barrier Switch........................ON (PROCEED WITH FLIGHT)
END
Ground Spoiler Failure AFM 4-15-50
INFLIGHT:
If the GND SPOILER warning message illuminates:
1. Ground Spoiler Arming Switch..................................................OFF
2. GND SPOILER Circuit Breaker (CPO, C-6)............................PULL
DURING LANDING:
If NO GND SPOILER light illuminates (remains ON) after landing
touchdown (GND SPOILERS ARMED):
1. Speed Brakes...........................................DEPLOY IMMEDIATELY
NOTE: AIRPLANE CONFIGURATION message may illuminate and
warning tone may sound momentarily.
NOTE: NO GND SPOILER light may light momentarily after touchdown
during landing, and then go out again, in less than one (1) second. This is
the normal sequence of events as the ground spoilers go through their
automatic deployment process. Wheel spin up logic should preclude this
occurrence. If light remains ON after touchdown, the above procedure
applies.
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EE - 5
Runaway Electric Pitch Trim AFM 3-15-60
In the event of runaway electric pitch trim:
1. Autopilot Disconnect Button .............................PRESS AND HOLD
If electric trim is disabled while switch is held:
2. Electric Pitch Trim ......................................................DISENGAGE
3. Autopilot Disconnect Button ............................................RELEASE
4. Manual Pitch Trim Wheel .................................... USE TO RETRIM
NOTE: Subsequent attempts to engage the autopilot will result in
automatic re-engagement of electric trim.
Alternate Procedure:
1. Manual Pitch Trim Wheel................................ GRASP AND HOLD
2. Electric Pitch Trim ......................................................DISENGAGE
NOTE: Subsequent attempts to engage the autopilot will result in
automatic re-engagement of electric trim.
END
Frozen Pitch Trim AFM 3-15-70
NOTE: If either or both FGCs have “hard failed” due to frozen trim, pull and
reset both FGC CBs (FGC #1: CPO, A-7; FGC #2: CPO, B-7).
If frozen pitch trim is suspected:
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：灣流4快速檢查單QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 3(40)