Some aircraft have a red guarded Smoke Detector switch
for each lavatory located at the adjacent Flight Attendant
panel. Move the switch to the OFF position.
(Continued)
If the red guarded smoke detector switch is not installed, locate the smoke detector unit under the sink area or in a compartment between the sink and toilet. Disconnect the cannon plug located on the smoke detector.
The affected lavatory must be locked and not used for the remainder of the flight. Make a logbook entry.
* * * *
APU FIRE (INFLIGHT) CHECKLIST
APU FIRE CONT Switch ........................................ OFF & AGENT ARM
Note: If APU does not shut down, pull APU CONTROL circuit breaker (overhead panel - battery bus).
APU FIRE AGENT Switch 1 OR 2 ..................................................DISCH
Check respective AGENT LOW light is on.
IF APU FIRE Light Is On After 30 Seconds:
Remaining APU FIRE AGENT Switch .....................................DISCH
APU MASTER Switch..........................................................................OFF
APU CONTROL Circuit Breaker (Battery Bus).............................. PULL
APU FIRE CONT Switch ................................................................ NORM
APU DOORS Switch..........................................................................AUTO
* * * *
INTENTIONALLY LEFT BLANK
MD-80 Flight Manual Continental Sec. 2 Page 77 Rev. 12/01/00 #29
APU FIRE (INFLIGHT) EXPANDED CHECKLIST
APU FIRE CONT Switch ........................................ OFF & AGENT ARM
Shuts off APU and completes circuit to APU fire agent switches.
Note: If APU does not shut down, pull APU CONTROL circuit breaker (overhead panel - battery bus).
APU FIRE AGENT Switch 1 OR 2 ..................................................DISCH
Check respective AGENT LOW light is on. Requires normal power.
IF APU FIRE Light Is On After 30 Seconds:
Remaining APU FIRE AGENT Switch .....................................DISCH
APU MASTER Switch..........................................................................OFF
This will assure fuel is not sent to the APU after the next step.
APU CONTROL Circuit Breaker (Battery Bus).............................. PULL
This will prevent inadvertent starting of the APU.
APU FIRE CONT Switch ................................................................ NORM
This will prevent inadvertent discharge of remaining fire agent.
APU DOORS Switch..........................................................................AUTO
This closes the APU doors.
* * * *
INTENTIONALLY LEFT BLANK
MD-80 Sec. 2 Page 79
Flight Manual Continental Rev. 05/15/95 #23
LOSS OF PRESSURIZATION / RAPID DECOMPRESSION / EMERGENCY DESCENT CHECKLIST
IMMEDIATE ACTION
Oxygen Masks, Regulators......................................................ON, 100% Crew Communications .................................................. ESTABLISHED NO SMOK, SEAT BELTS switches.................................................. ON
SECONDARY ACTION
PNF accomplish or verify and advise when completed:
CABIN ALT Control Lever, Wheel ..............................................................LOCKED DOWN, FULL FORWARD
Note: Manual control forces may be high. Apply force as required.
PNEU X-FEED VALVE Levers...................................................CLOSE
AIR CONDITIONING SUPPLY Switches ....................................AUTO
RADIO RACK Switch.......................................................................FAN
IF Cabin Altitude Is Below 14,000 Feet and Controllable:
CABIN ALT Control Lever, Wheel........................ AS REQUIRED
Return cabin pressure to that appropriate for flight altitude.
OR Descend as necessary to maintain cabin altitude below 14,000
feet.
* * * *
IF Cabin Altitude Is At Or Above 14,000 Feet Or Not Controllable:
Perform an emergency descent. Advise F/A’s as soon as possible.
Throttles..............................................................................CLOSED
Speedbrakes........................................................................EXTEND
Structural Integrity .................................................... DETERMINE
Descent Speed ...............................................................ESTABLISH
No Structural Damage/No Turbulence: .80-.82M/320-340 KIAS
Structural Damage or Turbulence: .75-.79M/275-285 KIAS
(Continued)
ATC ......................................................................................... ADVISE 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(40)
