Flaps ............................................................................................... 28°
Spoilers........................................................................ RETRACTED
CAB ALT Control Wheel, Lever....................FULL AFT (OPEN),
LOCKED DOWN
(Continued)
IF Evacuation Is Confirmed Necessary:
FUEL Levers..................................................................... OFF Passenger Evacuation..... “EASY VICTOR, EASY VICTOR”
EMER LTS Switch ............................................................. ON
BATT Switch..................................................................... OFF
ENG Fire Handles...........................................................PULL
- - - - -CREW EVACUATION DUTIES - - - - -
Captain: Assist Flight Attendants in forward cabin entry area. Open galley service door if unopened. Ensure all
OR
passengers and crew have evacuated the aircraft.
F/O: Deplane with cockpit fire extinguisher and release tail cone exit if unopened. Assist passenger evacuation at wing edge and direct passengers to assembly point.
Observer: If qualified, assist Flight Attendants in passenger evacuation.
* * * *
IF Evacuation Is Not Necessary:
EMER PWR Switch.......................................................... OFF
Continue at .
IF Emergency Evacuation Is Not Required:
. Identify malfunction and accomplish appropriate checklist, as required.
(Continued)
- - - - - AFTER PROBLEM IS STABILIZED - - - - -
Captain should make a “reassurance PA” to the passengers. Do not taxi until the Flight Attendants verify all passengers are seated and all doors/exits are closed.
After Landing Checklist ............................................ACCOMPLISH
Note: If tire damage is suspected, do not retract flaps.
Note: Prior to subsequent takeoff, re-accomplish all normal departure checklists beginning with the BEFORE START checklist.
Brake Temperatures.........................................................MONITOR
Note: Do not set parking brake if temperature is above 300.C.
IF Above 205.C But Less Than 400.C (305.C for MD-83):
Allow brakes to cool until temperature is below 205.C before
next takeoff.
OR
* * * *
IF Above 400.C (305.C for MD-83) And/Or OVHT Light Is On:
WARNING: Keep all personnel clear of main landing gear. If a 400.C (305.C for MD-83) temperature exists for approximately 5 minutes, wheel fuse plugs may activate and deflate the tires. Brakes, wheels, and tires will require maintenance inspection before next flight.
* * * *
INTENTIONALLY LEFT BLANK
REJECTED TAKEOFF EXPANDED
CHECKLIST
Tower/Ground..................................................................................NOTIFY
PASSENGER PA ....................“REMAIN SEATED, REMAIN SEATED”
Advise passengers to remain seated unless immediate evacuation is required.
IF Takeoff Rejected for Engine Fire:
Fire Warning Bell............................................................SILENCE
The F/O should silence the bell as soon as possible.
FUEL Lever (Affected Engine)................................................OFF
ENG FIRE Handle.....................................PULL & ROTATE TO (Affected Engine) AGENT DISCH 1 AND 2
Pull the appropriate ENG FIRE handle to the full aft stop and rotate left, then right to discharge both bottles. 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.
IF Takeoff Rejected for APU Fire:
APU FIRE CONT Switch .......................... OFF & AGENT ARM
Note: If APU does not shutdown, pull APU CONTROL circuit breaker on the overhead bus.
APU FIRE AGENT Switch 1.............................................. DISCH
Observe AGENT LOW illuminate (requires right DC bus).
APU FIRE AGENT Switch 2.............................................. DISCH APU MASTER Switch.............................................................OFF Caution: Do not use the aft emergency escape slide to evacuate
passengers if an APU fire is suspected.
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. Assure crash/fire/rescue coverage for taxiing.
(Continued)
Sec. 2 Page 48 MD-80
Rev. 01/01/97 #25 Continental Flight Manual
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