FIRST FLIGHT OF DAY
In accordance with FAR 121.576, each item of crew baggage carried in
the flight deck must be secured.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
BEFORE START CHECKLIST
The Capt will call for the BEFORE START CHECKLIST after all cabin doors are closed, all passengers are seated, and carry-on luggage is properly stowed. If a pushback is required, the checklist asterixed items will be completed prior to aircraft movement (down to the line). When engine start clearance is received, he/she will call for the rest of the checklist (below the line) and the appropriate engine to be started. In the event a pushback is not required, the entire checklist (above and below the line) will be completed prior to engine start.
BEFORE START F/O CHALLENGE * Prior to Aircraft Movement CAPT RESPOND
* Upper Wing Anti-Ice.........LIGHTS OUT / INSPECTION COMPLETE * Flight Papers, ZFW, Logbook................. CHECKED, SET, ON BOARD * Fuel & Pumps .....................____GATE FUEL, ___ ON BOARD, 4/6 ON * Pitot Heat & Ignition ......................... . ................................................ ON * Seat Belt & Beacon.................................................................................. ON * Hydraulics................................................................ ON & HI, CHECKED - - - -WHEN CLEARED TO START - - - - - -Galley Power & Packs........................ . .............................................. OFF PNEU X-Feeds, Pressure ................... . .....................OPEN, CHECKED . Right pack/x-feed only
F/O Challenge * Prior to Aircraft Movement Capt Respond
* Upper Wing Anti-Ice.........LIGHTS OUT / INSPECTION COMPLETE
Press to test the WING ICE ALERT and WING HTR INOP lights. Lights should
illuminate when pressed, and extinguish when released.
If the UWAI system is not installed, inoperative, or a light remains on
after test, ensure the wing ice inspection is completed and signed off in
the aircraft logbook.
* Flight Papers, ZFW, Logbook................. CHECKED, SET, ON BOARD
This step normally accomplished by the Capt. Verify that the dispatch release, flight plan, pre-departure clearance (if applicable), fuel slip, accuload, and logbook are checked and on board. The Captain may elect to pushback/start engines when assured that the final weight and balance is forthcoming.
Fuel slip and accuload procedures are discussed in the operations manual.
Push the ZFW knob on the fuel quantity display and rotate in the direction required to set the calculated zero fuel weight. Release the ZFW knob and the ZFW and fuel quantity will add up to the aircraft gross weight.
Ensure the logbook has no open writeups, the wing ice inspection is signed off (if required), and the “First Flight of the Day” checks are signed off with the appropriate date on the “R’qrd A/C Checks” line.
* Fuel & Pumps....................____GATE FUEL, ____ON BOARD, 4/6 ON
This step normally accomplished by the Capt. Check the fuel on board against the dispatch release, fuel slip, and accuload. Turn on both boost pumps in each wing tank and observe that both INLET FUEL PRESS annunciator lights are extinguished. If the center tank contains useable fuel, turn on both center tank boost pumps and leave them on until center fuel tank has been emptied.
Note: All auxiliary tank fuel transfer pumps must be off for takeoffs and landings.
* Pitot Heat & Ignition ......................... . ................................................ON
This step normally accomplished by the Capt (F/O on restart). Place METER SEL & HEAT switcht to CAPT position. Place IGN switch to SYS A going away from origination airport and SYS B coming back (GRD START & CONTIN on some aircraft).
* Seat Belt & Beacon..................................................................................ON
This step normally accomplished by the Capt. Turn the SEAT BELTS and
ANTI COLLISION switches to ON.
* Hydraulics................................................................ ON & HI, CHECKED
This step normally accomplished by the F/O. Auxiliary and transfer hydraulic pumps are selected ON, engine driven hydraulic pumps remain in HIGH, to provide maximum system hydraulic pressure for braking during the pushback and engine start procedure. 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(138)
