Sec. 4 Page 102 Rev. 01/01/00 #28 Continental MD-80 Flight Manual
TAKEOFF PROCEDURE CHART ALTERNATE NOISE ABATEMENT PROFILE (ICAO A)
STANDARD NOISE ABATEMENT TAKEOFF PROFILE ALTERNATE NOISE ABATEMENT TAKEOFF PROFILE
(U.S. Close-in / ICAO Profile A)
AFTER TAKEOFF CHECKLIST
The Pilot Flying will call for the AFTER TAKEOFF CHECKLIST in conjunction with the slats retract call. Do not allow the reading of the checklist to interfere with outside vigilance while departing the terminal area.
Caution: To avoid the possibility of the shoulder harness buckles snapping back and inadvertently pulling circuit breakers, hold both straps before releasing and then allow the straps to retract slowly to the stowed position.
PILOT MONITORING PILOT MONITORING CHALLENGE AFTER TAKEOFF RESPOND
Gear.................................................................................. UP, LIGHTS OUT Flaps, Slats............................ [AS REQ] .....UP, LIGHTS OUT, STOWED Ignition............................................................................................ ON / OFF Fuel Feed .......................................CK/BAL ....................CENTER / MAIN Hydraulics ............................ [AS REQ] ................................. OFF & LOW Spoilers, Autobrake System ............................................DISARMED, OFF [AS REQ] on Missed Approach
PM CHALLENGE PM RESPOND Gear.................................................................................. UP, LIGHTS OUT
The PM will raise the landing gear handle on command of the PF after a positive rate of climb has been verified on the IVSI & barometric altimeter, and called by either pilot. Verify that no red lights are illuminated and that the GEAR DOOR OPEN light is out.
Flaps, Slats............................ [AS REQ] .....UP, LIGHTS OUT, STOWED
At the applicable flap retraction speed, retract the flaps. Move the flap/slat handle to 0° and observe both flap position pointers start to move symmetrically toward up.
Note: If the flap pointers do not move or do not move together, return the flap/slat handle to the previous position and refer to the abnormal procedures section.
At the applicable slat retraction speed, retract the slats. Move the flap/slat handle to UP/RET and observe that all the lights on the slat position indicator panel are out. If used during takeoff, the flap takeoff selector should be rotated to the STOW position.
For missed approach, flaps and slats may be used as desired.
Ignition..............................................................................................ON / OFF
The ignition switch should be turned off as soon as the engines have stabilized. For optimum life of the ignition system components, the duty cycle is 10 minutes on and 10 minutes off. However, when adverse flight conditions are encountered such as ice or water ingestion, turbulence, or conditions which could result in engine flameout, it is recommended that the two halves of the 20 joule A/C ignition system should be used in alternating 10 minute periods for as long as needed to ensure against engine flameout. It should be recognized that prolonged use of the ignition system reduces its service life.
Note: On aircraft so equipped, there is no time limit for the Ground Start and Continuous position.
Fuel Feed .......................................CK/BAL ..................... CENTER / MAIN
All main tank boost pumps will be on for the duration of the fight.
If center tank fuel is available, leave both CTR tank pumps on. If auxiliary tank fuel is available, move FWD and AFT AUX TRANS switches to AUTO. Confirm center tank is feeding by observing main tank and center tank fuel quantities. If center tank is not feeding, refer to CENTER FUEL TANK DOES NOT FEED, Section 3. Check main tank balance.
When auxiliary tanks are empty move FWD and AFT AUX TRANS switches to
OFF. When center tank is empty, move CTR tank pump switches to OFF.
The actual configuration will be announced in the checklist response,
"FEEDING FROM THE CENTER (or MAIN) TANKS."
Hydraulics ............................ [AS REQ] ................................... OFF & LOW
After the flaps and slats are retracted, move the L & R ENG HYD PUMP 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 2(3)
