曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
RETRACTION FOLLOWING ALTERNATE EXTENSION COULD RESULT
IN A GEAR UP LANDING.
CAUTION: THIS RESET/RETRACTION PROCEDURE IS PROVIDED
FOR USE IF GREATER OR COMPOUNDED EMERGENCY CONDITIONS
EXIST AND IS NOT TO BE CONSIDERED AUTHORIZATION TO
RECYCLE LANDING GEAR AFTER ROUTINE MAINTENANCE OR
TRAINING USE OF THE BLOW DOWN SYSTEM.
1. Landing Gear Handle ...........................................................DOWN
2. Emergency Landing Gear T-Handle..........................PUSH DOWN
Push handle down to assure handle is fully seated. Wait minimum
of thirty (30) seconds after reseating handle to allow pressure to
bleed off.
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EG - 6 May 30/02
Landing Gear Alternate Operation, ctd… AFM 3-19-20
3. Dump Valve D-Ring ................................................................PULL
NOTE: Handle must be pulled up fully, held for ten (10) seconds,
then restowed.
4. Landing Gear Handle ..................................................................UP
NOTE: There is no backup method for retracting landing gear.
END
Nose Wheel Steering Failure AFM 3-19-30
If the STEER BY WIRE FAIL amber caution message illuminates
on CAS, proceed as follows:
For airplanes SN 1000 thru SN 1143 without ASC 176:
1. Nose Wheel Steering Switch .................................OFF, THEN ON
2. If Message Stays On: Nose Wheel Steering Switch.................OFF
3. Use brakes, rudder, and/or differential power for directional control.
NOTE: Normal shimmy damping will be available with nose wheel
steering OFF.
IF AIRBORNE:
For airplanes SN 1144 and subs. or airplanes with ASC 176:
NOTE: Message will only illuminate with landing gear extended.
After Takeoff:
1. Nose Wheel Steering Switch ....................................................OFF
If the nose steering wheel is NOT centered, leave landing gear
DOWN and land as soon as practical.
If the nose steering wheel is centered, remove feet from rudder
pedal(s) and hands-off nose steering wheel.
2. Landing Gear ..................................................................RETRACT
On Approach:
1. Nose Wheel Steering Switch ....................................................OFF
Continued on next page →
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EG - 7
Nose Wheel Steering Failure, ctd… AFM 3-19-30
After Landing:
1. Nose Wheel Steering Switch......................................................ON
A. If message extinguishes, expect normal nose wheel steering
output.
B. If message remains ON, use brakes, rudder, and / or differential
power for directional control.
END
Nutcracker System Fails To Shift To Ground Mode At
Touchdown AFM 3-19-40
For airplanes with ASC 166:
1. Red REV UNLOCK message will illuminate with the use of thrust
reversers. Thrust reversers will stow at low ground speed.
2. Ground spoilers will deploy with wheel spin-up, but will retract at low
ground speed.
3. Anti-skid system may not operate normally. Be prepared to turn
anti-skid off at low ground speed if you lose brakes.
4. Engine idle will go to 67% HP at low ground speed.
5. APU air is inoperative.
6. Pressurization outflow valve will not open automatically. Switch to
manual and open outflow valve.
7. Stick shaker and pusher remain armed.
8. Landing gear handle is not safe (safety solenoid energized).
9. Engines cannot be restarted.
For airplanes without ASC 166:
1. Thrust reversers are inoperative.
2. If speed brakes are used, a red ACFT CONFIG message will
illuminate.
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EG - 8 May 30/02
Nutcracker System Fails To Shift To Ground Mode At Touchdown,
ctd… AFM 3-19-40
3. Ground spoilers will deploy with wheel spin-up, but will stow at low
ground speed.
4. Anti-skid system may not operate normally. Be prepared to turn
anti-skid off at low ground speed if brakes are lost.
5. Engine idle will go to 67% HP on landing.
6. Pressurization outflow valve will not open automatically. Switch to
manual and open outflow valve.
7. APU air is inoperative.
8. Stick shaker and pusher remain armed.
9. Landing gear handle is not safe (safety solenoid energized).
10. Engines cannot be restarted.
END
Nutcracker System Fails To Shift To Air Mode After
Takeoff AFM 3-19-50
WARNING: THRUST REVERSERS ARE OPERATIVE IN FLIGHT IF
POWER LEVERS ARE RETARDED TO IDLE.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 3(49)
