IF Engine Fire Or Severe Damage Is Suspected:
ENG FIRE Light Is Out After 10 Seconds And Severe Damage Is Not Suspected:
Test fire warning system. Continue idle engine operation at Captain’s discretion.
* * * *
ENG FIRE Light Is On Or Severe Damage Is Suspected:
FUEL Lever (Affected Engine)........................................ OFF
ENG FIRE Handle (Affected Engine) ..........................PULL AND ROTATE TO AGENT DISCH 1 OR 2
Check respective AGENT LOW Light is on. IF Fire Persists After 30 Seconds:
ENG FIRE Handle (Affected Engine) ............... ROTATE TO DISCHARGE REMAINING AGENT
Test fire warning system. Continue checklist at .
IF Engine Failure Or Inflight Shutdown:
Note: Consider operating engine at idle thrust for two minutes for precautionary shutdowns.
FUEL Lever (Affected Engine)...................................................... OFF
. ENG IGN Switch......................................................... AS REQUIRED
OVRD position should not be used because it would operate igniters
in the shutdown engine.
APU ..................................................................................................START
(Continued)
FUEL X-FEED Lever, Boost Pumps
(If No Center Wing Fuel)...............................................ON, PUMPS SET
PNEU X-FEED VALVE Lever (Affected Engine)........................CLOSE
AUX & TRANS HYD PUMP Switches ........................... AS REQUIRED
AIR CONDITIONING SUPPLY Switch (Affected Engine)..............OFF
AIR COND SHUTOFF Switch........................................................OVRD
ENG SYNC Selector ........................................................................... OFF
APU Bus Switch (Affected side) ........................................................... ON
IF Driftdown is Required:
Refer to DRIFTDOWN PROCEDURE.
IF Engine Restart is to be Attempted:
Refer to INFLIGHT ENGINE START CHECKLIST.
IF After Takeoff or Missed Approach: Accomplish the After Takeoff checklist.
Refer to ONE ENGINE INOPERATIVE APPROACH AND LANDING CHECKLIST.
* * * *
ENGINE FAILURE / FIRE / SEVERE DAMAGE /
INFLIGHT SHUTDOWN EXPANDED CHECKLIST
This procedure is to be used for engine failure, engine fire, engine severe damage (including separation), or shut down for precautionary reasons.
Note: A fire warning may or may not appear with severe engine damage or separation. Indications of severe damage may include airplane vibration and, on the affected side, N1 and/or N2 tachometers indicating 0%, rapid loss of hydraulic pressure and sudden loss of generator power.
Fire Warning Bell (If Applicable)...............................................SILENCE
The PM should silence the bell as soon as possible.
Autothrottles ....................................................................... DISENGAGED
This action prevents undesired autothrottle activity.
Throttle (Affected Engine)............................................................CLOSED
IF Engine Fire Or Severe Damage Is Suspected:
ENG FIRE Light Is Out After 10 Seconds And
Severe Damage Is Not Suspected:
Test the fire warning system. A valid test with no other
OR indication of a fire indicates a possible engine bleed air leak.
Continue idle engine operation at Captain’s discretion.
* * * *
ENG FIRE Light Is On Or Severe Damage Is Suspected:
FUEL Lever (Affected Engine) ........................................... OFF
Note: This action must be verified by the other pilot.
ENG FIRE Handle (Affected Engine)..............................PULL AND ROTATE TO AGENT DISCH 1 OR 2
Note: This action must be verified by the other pilot.
(Continued)
Pull the appropriate ENG FIRE handle to the full aft stop and rotate simultaneously to discharge a bottle. A slight increase in force will be felt during the last . inch of aft travel. The handle load should not be relaxed until the respective AGENT LOW light is on. Start a clock for timing.
IF Fire Persists after 30 Seconds:
ENG FIRE Handle (Affected Engine)...................ROTATE TO DISCHARGE REMAINING AGENT
If fire light extinguishes during this procedure, it is recommended that a fire warning system test be conducted to verify fire detection system is functioning normally.
Continue checklist at .
IF Engine Failure Or Inflight Shutdown:
Note: Consider operating engine at idle thrust for two minutes for precautionary shutdowns.
FUEL Lever (Affected Engine)...................................................... OFF
Note: This action must be verified by the other pilot.
. ENG IGN Switch......................................................... AS REQUIRED
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：MD-80 Flight Manual 麦道80飞行手册 1(21)
