If GPU available, accomplish appropriate checklist.
BATT Switch & EMER PWR Switch....................................................ON
Accomplish applicable items on the BEFORE START Checklist, Sect. 4.
DC Start Pump........................................................................................ON
Communications..............................................................................CHECK
DONOR AIRCRAFT:
Main Wheel...............................................................................CHOCKED
Before Start Checklist ....................................................... ACCOMPLISH
Right Engine ....................................................................................START
AUX Hydraulic Pump.............................................................................ON
APU Bleed Air Switch .......................................................................... OFF
Right PNEU X-FEED VALVE Lever................................................ OPEN
Left PNEU X-FEED VALVE Lever.............................................CLOSED
Communications..............................................................................CHECK
Caution: APU may be used as the source of air only if no other air source
is available.
(Continued)
MD-80 Sec. 3 Page 123
Flight Manual Continental Rev. 05/15/96 #24
- - - - - START SEQUENCE - - - - -
RECIPIENT AIRCRAFT DONOR AIRCRAFT
Start right engine by operating Start Switch, call “AIR ON.”
Advance power to maintain 40 psi on pneumatic gauge.
At 40% N2 release Start Switch, call “AIR OFF.”
Reduce power to idle.
When engine is stabilized, call “START COMPLETED.” Close right crossfeed valve.
Close right crossfeed valve and open left crossfeed valve.
Note: OIL PRESSURE LOW light, N1, EGT, and N2 will be operative during start. Immediately after generator comes on line, check that start valve open light is out.
* * * *
CROSSBLEED START
Ramp Area.................................................................................... CLEAR
Taxi away from the terminal on one engine, clear the area, then make the crossbleed start.
Parking Brake......................................................................................SET
PNEU X-FEED VALVE Levers .......................................... BOTH OPEN
Operating Engine Throttle......................................................ADVANCE
Advance the throttle to obtain necessary pneumatic pressure for starting.
Opposite Engine.............................................................................START
Using normal starting procedures start non-operating engine. At starter release, reduce throttle to idle on operating engine.
* * * *
Sec. 3 Page 124 MD-80
Rev. 08/01/98 #27 Continental Flight Manual
ENGINE CLEARING PROCEDURE
FUEL Lever ........................................................................................ OFF
Throttle ............................................................................................. IDLE
N2 ...................................................................................................ZERO
Indicates rotation has ceased.
IF Aircraft 870 Or 872-879:
ENG IGN Switch.......................................................................... OFF
IF Other than aircraft 870 Or 872-879:
ENG IGN Switch.........................................SYS A, SYS B, or BOTH
START Switch .............................. ON, HOLD FOR 20 SECONDS, OFF
* * * *
HOT START
Note: Fuel flow above 1100 pph. may indicate an impending hot start. If initial fuel flow is high, monitor EGT closely.
FUEL Lever ........................................................................................ OFF
ENG START Switch........................... HOLD FOR 10 TO 15 SECONDS
Caution: If start switch has been prematurely released, do not reposition to on. Refer to ENGINE CLEARING PROCEDURE, this section.
ENG START Switch...........................................................................OFF
ENG IGN Switch ................................................................................ OFF
Note: Do not attempt restart until maintenance inspection completed. Note maximum EGT during start.
* * * *
MD-80 Sec. 3 Page 125
Flight Manual Continental Rev. 12/01/00 #29
HUNG START
Note: This condition is indicated when engine does not continue
acceleration to idle.
ENG HYD PUMP Switch (Affected Engine)................................. OFF 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(98)
