Parking Brake........................................................................SET
Tower/Ground............................................................CONTACT
Advise tower and/or ground crew of abnormal airplane conditions, possibility of evacuation, and planned evacuation routes.
EMER PWR Switch..................................................................ON
This assures uninterrupted power source for the Captain’s evacuation PA through the handset.
Flaps .......................................................................................... 28°
This aids in overwing passenger evacuation.
Spoilers....................................................................RETRACTED
This lowers the spoiler panels to prevent interference with passenger evacuation.
CAB ALT Control Wheel, Lever .................FULL AFT (OPEN), LOCKED DOWN
This insures aircraft is depressurized for operation of exits.
IF Evacuation is Confirmed Necessary:
FUEL Levers .................................................................... OFF Passenger Evacuation....“EASY VICTOR, EASY VICTOR”
Note: If evacuation routes must be restricted, advise Flight Attendants of the correct routes prior to Easy Victor
OR
call.
The Captain shall order the evacuation in the following manner: “THIS IS THE CAPTAIN (state the useable exits) EASY VICTOR, EASY VICTOR”.
EMER LTS Switch.............................................................ON
BATT Switch....................................................................OFF
ENG Fire Handles......................................................... PULL
~
(Continued)
~
- - - - -CREW EVACUATION DUTIES - - - - -
Captain: Assist Flight Attendants in forward cabin entry area. Open galley service door if unopened. Ensure all 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.
- - - - - 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.
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.
* * * *
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.
* * * *
MD-80 Sec. 2 Page 51
Flight Manual Continental Rev. 08/01/98 #27
REJECTED TAKEOFF PROCEDURE
A Rejected Takeoff (RTO) is a maneuver performed during the takeoff roll to expeditiously stop the aircraft on the runway.
The Captain is responsible for making the rejected takeoff decision and performing the rejected takeoff maneuver. The First Officer must monitor all takeoffs for any abnormality which might be cause for rejecting a takeoff, and be prepared to act in the event the Captain becomes incapacitated.
The rejected takeoff decision must be made, and (if rejecting) the rejected takeoff maneuver initiated, before reaching V1. The following table lists reject criteria for the low speed portion (below 100 knots) and high speed portion (above 100 knots) of takeoff roll.
REJECTED TAKEOFF CONSIDERATIONS
BELOW 100 KNOTS ABOVE 100 KNOTS
Engine Failure/Fire Unsafe Configuration Unsafe/Unable to Fly Cabin Smoke/Fire System Failure Unusual Noise or Vibration Tire Failure Abnormal Acceleration Windshear Warning Engine Failure Unsafe Configuration Unsafe/Unable to Fly . Maximum braking required to a full stop . The aircraft will remain on the runway until completion of the REJECTED TAKEOFF CHECKLIST
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