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4. Emergency Flap Control...................................................................
................................... PUSH OR PULL (EXTEND OR RETRACT)
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EE - 8 May 30/02
Wing Flaps - Alternate Operation, ctd… AFM 3-14-20
When flaps attain desired position:
5. Emergency Flap Control .................................................NEUTRAL
CAUTION: IN ORDER TO GUARD AGAINST THE REMOTE
POSSIBILITY OF ASYMMETRY PROTECTION FAILURE WHEN USING
EMERGENCY FLAP CONTROL, OBSERVE THAT NO AIRPLANE ROLL
IS PRESENT INDICATING FLAP ASYMMETRY. IF ASYMMETRY IS
INDICATED, RETURN FLAPS TO THEIR PREVIOUSLY SELECTED
POSITION.
END
Partial Flaps Landings AFM 3-14-30
If landing at a reduced flap setting is unavoidable, fly a wide
approach and select the longest available runway. Once
established:
1. Airstart Ignition ........................................................................... ON
2. VREF ..................................APPROPRIATE TO CONFIGURATION
Landing with less than full flaps negates ground spoiler deployment
as result of wheel spin-up unless the Ground Spoiler Flap Override
switch is selected ON before landing. Ground spoiler deployment
as result of weight-on-wheels should be normal.
CAUTION: TIRE SPEED LIMITATIONS WILL BE EXCEEDED IF
TOUCHDOWN IS MADE IN EXCESS OF 182 KNOTS GROUND SPEED.
(195 KNOTS GROUND SPEED SN 1214 AND SUBS., AND SN 1000
THRU 1213 WITH ASC 190.)
END
Undesired Flap Movement AFM 3-14-40
In the event of uncontrolled flap movement:
1. Emergency Flap Switch ......................................................EMERG
Continued on next page →
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EE - 9
Undesired Flap Movement, ctd… AFM 3-14-40
2. Emergency Flap Control...................................................................
................................... PUSH OR PULL (EXTEND OR RETRACT)
3. MANUAL FLAP CONT Circuit Breaker (CPO, A-1) ................PULL
NOTE: With MANUAL FLAP CONT circuit breaker pulled, flaps are
inoperative. Emergency flap control may be regained by resetting
MANUAL FLAP CONT circuit breaker and operating the Emergency Flap
Control.
END
Autopilot Malfunction AFM 3-03-10
If the autopilot malfunctions, disengage autopilot as follows:
1. Autopilot Disengage Button (Either Pilot’s Control Wheel)...............
.............................................................. PRESS (MOMENTARILY)
The autopilot may also be disengaged by any of the following:
2. Autopilot "ON" Capsule (Guidance Panel) .......................... PRESS
3. Electric Elevator Trim Switch...........................................ACTUATE
4. Either Go-Around (G/A) Button ........................................... PRESS
CAUTION: THE AUTOTHROTTLE, IF ENGAGED WHEN THE G/A
BUTTON IS PRESSED, WILL INCREASE POWER TO G/A EPR.
If a flight guidance computer fails, the second computer will
continue to control airplane. A failure of the second computer will
disconnect the autopilot.
In the event that above methods fail, the autopilot may be
overpowered by the pilot.
END
Autothrottle Malfunction AFM 3-03-20
Disengage the autothrottle as follows:
1. Activating either momentary action engage/disengage thumb lever
located on the power levers.
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EE - 10 May 30/02
Autothrottle Malfunction, ctd… AFM 3-03-20
2. Activating either mechanical disengagement button located on the
front of the power lever knobs.
3. Deselecting the autothrottle ARM button on the guidance panel.
END
AFGCS Failure AFM 3-03-30
Fail Operational: If monitors detect a failure condition within a flight
guidance computer, the failed computer will be shut down and control
of the airplane will be transferred to the remaining computer.
Fail Passive: If the airplane is being controlled by the second flight
guidance computer, after a single failure, and that computer fails, the
autopilot will disengage.
END
Mach Trim Compensation Failure AFM 3-03-40
1. Pitch Trim Switch ....................................................... DISENGAGE
NOTE: Since electric elevator trim is not available, the manual trim
wheel must be used.
2. MMO.....................................................................LIMIT TO 0.75 MT
CAUTION: WHEN OBSERVING MMO OF 0.75 MT, CLOSELY
MONITOR AIRSPEED TO AVOID EXCEEDING 0.75 MT.
　
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