SPOILER FLOAT CHECKLIST
IF Rapid Roll Rate Develops During Extension of Flaps Beyond 28.:
FLAP/SLAT Handle .....................................RETRACT TO 28 / EXT
Adjust speed as required.
* * * *
Temporary Revision Sec. 2 Page 101 MD-80 Rev. 01-01 04/16/01 Continental Flight Manual
RUNAWAY STABILIZER CHECKLIST
Note: Do not oppose runaway using LONG TRIM handles. SECONDARY ACTION LONG TRIM Indicator Movement Stops Or Continues Runaway:
STABILIZER TRIM (Red Guarded) Switch ..............................................STOP ALT LONG TRIM Switch ..................................................................... RETRIM PRIMARY LONGITUDINAL TRIM
Circuit Breakers - Left Generator Bus - Row 4 ............................. PULL
Continue flight using alternate trim system. Autopilot is available.
* * * *
LONG TRIM Indicator Movement Reverses:
AUTOPILOT AND ALTERNATE LONGITUDINAL TRIM Circuit Breakers D-09,10,11 (D-04, 05, 06/08, 09, 10/10, 11, 12) ............................... PULL
Continue flight using primary trim system. Autopilot is available, but autotrim function is inoperative. After trimming, autopilot may be engaged, but should be disconnected / retrimmed periodically as needed.
* * * *
INTENTIONALLY LEFT BLANK
Temporary Revision Sec. 2 Page 103 MD-80 Rev. 01-01 04/16/01 Continental Flight Manual
RUNAWAY STABILIZER EXPANDED CHECKLIST
Caution: A runaway trim condition resulting in the stabilizer trimming to the full NOSE UP position may require establishing a steep bank angle to control pitch.
Caution: Avoid manual pitch inputs until the autopilot is disconnected.
Note: Extended trim operation may result in trim motor thermal shutdown. Trim motor operation may return after sufficient cooling period.
IMMEDIATE ACTION
Autopilot .......................................................................DISCONNECT Control Wheel Trim Switches .............................. TRIM OPPOSITE DIRECTION OF RUNAWAY
Note: Do not oppose runaway using LONG TRIM handles.
SECONDARY ACTION
LONG TRIM Indicator Movement Stops or Continues Runaway:
STABILIZER TRIM (Red Guarded) Switch ..............................................STOP
This switch interrupts power to the primary motor brake release and applies the brake. It does not interrupt electrical power to the primary trim motor and does not affect the alternate trim brake or motor. If the runaway was caused by the primary system, movement of the stabilizer will stop because the motor is not capable of overcoming the brake.
OR ALT LONG TRIM Switch ..................................................................... RETRIM PRIMARY LONGITUDINAL TRIM
Circuit Breakers - Left Generator Bus - Row 4 ............................. PULL
This will prevent the primary trim motor from overheating. Continue
flight using alternate trim system. Autopilot is available.
* * * *
LONG TRIM Indicator Movement Reverses:
AUTOPILOT AND ALTERNATE LONGITUDINAL TRIM Circuit Breakers D-09,10,11 (D-04, 05, 06/08, 09, 10/10, 11, 12) ............................... PULL
(Continued)
Temporary RevisionMD-80 Sec. 2 Page 104 Flight Manual Continental Rev. 01-01 04/16/01
If trim runaway occurs when autopilot is engaged, the malfunction may be caused by the autopilot trim coupler.
Continue flight using primary trim system. Autopilot is available, but autotrim function is inoperative. After trimming, autopilot may be engaged, but should be disconnected / retrimmed periodically as needed.
* * * *
TAIL COMPT TEMP HIGH LIGHT ON CHECKLIST
PNEU X-FEED VALVE Levers ............................................CLOSED
AIR FOIL Anti-Ice Switch(es).......................................................OFF
AIR CONDITIONING SUPPLY Switches.....................HP BLD OFF
Caution: If icing conditions are encountered with wing anti-ice off in excess of 2 minutes, refer to AIRFOIL ICE PROTECTION INOPERATIVE, Section 3. Light is Out (After 2 Minutes) And Airfoil Anti-ice is Not Required:
* * * *
IF Landing is Imminent (5 Minutes From Touchdown):
Continue approach. Use minimum power settings if light is on. 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 1(46)
