2.
EPR in excess of max allowable.
3.
“80 KNOTS.”
Note: If during any landing, tire damage is suspected, leave the flaps extended to prevent possible flap or engine damage. In an emergency, maximum reverse thrust, up to takeoff EPR, is authorized, however, under normal circumstances, reverse thrust use on landing will be limited to 1.6 EPR and be at forward idle thrust by no later than 60 knots.
Transfer of Aircraft Control
The Captain will assume control of the aircraft no later than when the aircraft departs the runway centerline for the purpose of exiting the runway.
AFTER LANDING CHECKLIST
The After Landing procedure is initiated by the First Officer after the aircraft has cleared the runway. When time permits, and after clearing all active runways, the Captain will call for the AFTER LANDING CHECKLIST. The First Officer will verify that all items have been accomplished, and will report “AFTER LANDING CHECKLIST COMPLETE.” The First Officer will not read the challenges and responses aloud. In the event any individual item(s) are not accomplished, the First Officer will bring those items to the attention of the Captain.
F/O CHALLENGE F/O RESPOND (SILENT) AFTER LANDING (SILENT)
Pitot Heat & Ignition................................................................................ OFF Ice Protection, Exterior Lights .............................................AS REQUIRED Flaps............................................................................................................. 15° Radar, TCAS.................................................................................OFF, STBY Spoilers, Autobrake System .......................................... RETRACTED, OFF
F/O CHALLENGE F/O RESPOND Pitot Heat & Ignition..............................................................................OFF Ice Protection, Exterior Lights ...........................................AS REQUIRED
Engine anti-ice is turned off unless icing conditions exist on the ramp. If engine anti-ice is used during taxi-in, it should be turned off at engine shutdown. Airfoil anti-ice is turned off.
Landing lights should always be retracted to avoid damage by ground
equipment.
Flaps............................................................................................................15°
Retract flaps to 15° for taxi-in. This will minimize FOD damage to the
engines.
Radar, TCAS...............................................................................OFF, STBY
WARNING: Failure to return the transponder to STBY after landing allows the radar to operate in the windshear mode creating a radiation hazard to personnel on the ground. The RDR-4B radiation hazard area extends 13.4 feet from the radar antenna in a 120 degree arc left and right of the aircraft centerline. This hazard exists even if the radar mode is selected OFF or TEST.
Spoilers, Autobrake System ........................................ RETRACTED, OFF
Push spoiler lever down and forward to fully retract the spoilers. Move
autobrake selector off.
AFTER LANDING NOTES
Engine Shutdown After Landing
Single engine taxi-in is authorized. The Captain should consider factors such as aircraft weight, gate and ramp congestion, proximity to concourse structures, ramp/taxiway slope, and taxi time to decide whether single engine taxi-in is appropriate.
Note: Single engine taxi is not recommended during conditions of reduced traction such as standing water, slush, snow, or ice.
If a power setting of more than 1.2 EPR is required to maneuver or the ramp/taxiways are slippery, two engine taxi procedures should be used.
Notes: The left engine hydraulic pump, the auxiliary hydraulic pump, and the transfer pump must all be operative for single engine taxi.
The First Officer will monitor brake pressure and quantity.
The left engine (or APU) generator must be operative.
Pratt & Whitney advise that shutting down an engine without a cool-down period increases the potential for coke to form in the oil system. Recommend delaying engine shutdown until approximately 3 minutes after landing, or gate arrival (whichever occurs first), for engine cooling.
Do not use this procedure if the right engine has been operated above 85% N2 for a period exceeding one (1) minute just prior to shut down. If these parameters are exceeded, operate the engine at idle for 5 minutes for temperature stabilization.
中國航空網 m.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(31)
