.
Crash, fire and rescue assistance availability.
.
An airport where major generator, hydraulic pump or engine change capability exists; specifically, LAX, DEN, IAH or ORD.
Caution: Do not let the emergency progress long enough to prevent
making a safe landing. On-time performance to scheduled
destination must be sacrificed for safety, so land as soon as
practicable.
The flight crew can expect any or all of the methodikal emergencies to progressively develop in the following manner:
Series Of Rings...........................................METHODIKAL CHECKLIST
Overhead Speakers...............................................................................OFF
Headsets ..................................................................................................ON
D. C. X-Tie ......................................................................................... OPEN
Left Generator ............ OFF (MASTER CAUTION & AMBER LIGHTS)
Generator failed, however safe airplane flying time limited to 1 hour on 1 generator.
(Continued)
Avoid weather conditions. Critical safety of flight instruments, radios and electrical sub-systems will be inoperative at this time.
Request any clearance to descend to MEA, or 10,000 feet. Advise ATC to notify CAL dispatch of Delta One Emergency (ELECTRICAL D #1)
At MEA, Or 10,000 Feet Airspeed ............................ REDUCE: 230 KIAS
Flap Lever..........................................................................15.
/ TAKEOFF
Monitor right engine for vibration. If generator bearing failure is the cause, or additional engine trouble develops:
No. 2 Throttle ......................................................... REDUCE POWER
Note: When the throttle is moved toward the closed position. A steady warning horn will sound. Maintain enough power from affected engine to sustain flight.
(Engine D #2)
Call ATC. Declare a Delta Two Emergency. Request CAL Dispatch be advised. Monitor cabin pressure control. Right engine delta three compressor flow control valve may not remain controllable. Cabin altitude and temperature control may vary. Attempt manual mode of operation for pressurization.
(Environment D #3)
Caution: Longitudinal yaw, Vertical pitch or Dutch roll problems may result from a combination of asymmetrical engine power and limited hydraulic power.
Use normal in-range approach and landing checklists.
APU Air Switch..............................................................................OFF
APU ...........................................................................................START
Left APU Bus Switch .......................................................................ON
Note: APU blue power in use lights on the indicators 15 minutes maximum.
(Continued)
Captain may exercise emergency authority to operate engine at power setting required to effect a safe landing.
Failed Engine .................................... THROTTLE, AS NECESSARY
Gear Down ............................................................................ 3 GREEN
Flaps ................................................................................................. 28.
The stall warning horn will be activated on the Delta Four final approach at approximately 5 knots above irreversible flight control stall. Exercise extreme caution down to touchdown.
(Flight Controls D #4)
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本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊(cè) 1(61)
