Decelerate in level flight until appropriate speed is attained. FGS IAS
Hold mode may be used to hold speed during descent.
Speed ................................................... ABOVE FL 180 = GW + 120 KIAS BELOW FL 180 = GW + 80 KIAS
Note: GW + 80 KIAS is below clean maneuvering airspeed. Limit bank angle to 15. or less.
Descent ............................................................................................. BEGIN
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INTENTIONALLY LEFT BLANK
ONE ENGINE INOPERATIVE APPROACH
AND LANDING CHECKLIST
Plan a flaps 28. landing with final approach flown at VREF + 10 for go-around capability. After ENGINE FAILURE/FIRE CHECKLIST is complete, use both throttles together for the remainder of the flight.
Note: All of the following checklists should be accomplished whenever returning for an engine out landing.
- - - - -IN-RANGE CHECKLIST - - - - -
Hydraulics.........................................C+F.............ON & HI, CHECKED
WARNING: Hydraulic pumps must be set to ON & HI for the landing gear and flaps to function normally.
Altimeters..........................................C+F ...................................____SET
FUEL Boost Pumps, Quantity ................................. #___ON, CHECKED
Maintain lateral fuel balance by crossfeeding as required.
Landing Data, Bugs..........................C+F.....................CHECKED, SET
Target speed will be flaps 28. VREF plus wind additive (minimum 10 knots for go-around capability). The wind additive is . steady state wind, plus all the gust, not to exceed an additive of 20 knots.
SEAT BELTS Switch............................................................................ ON
Pressurization & Anti-Ice....................................................................SET
Approach Briefing, Harness.........................................COMPLETE, ON
A normal approach briefing should be accomplished as early as practical. The autopilot will not be used for approach with an engine out and use of autothrottles is not recommended. Avoid getting low on short final.
When landing is assured, the rudder trim must be centered (no later than nose gear touchdown). After spoiler deployment and nose gear touchdown, deploy both engine reversers and use reverse thrust cautiously. Directional control should be maintained with rudder and differential braking, not by use of asymmetric reverse thrust. If directional control problems arise, return throttles to forward idle.
(Continued)
Go-Around Procedure...................................................................REVIEW
Note: Recommend coordinating straight ahead or simplified climb out instructions in the event of missed approach.
Accomplish a normal flaps 15. go-around except:
.
In Mexico City or similar high altitude airports, use flaps 11..
.
Climb at go-around speed on speed cards to 800 feet or obstacle clearance height and perform acceleration and cleanup as described in GO-AROUND (ONE ENGINE INOP) PROCEDURE.
- - - - - APPROACH CHECKLIST - - - - -
Altimeters & Bugs...............................C+F .......................................... SET
Radios, Course ................................................... IDENTIFIED, INBOUND
VOR/ADF & Marker Switches ............................................................ SET
- - - - - WHEN CLEARED FOR THE APPROACH - - - - -
Boost Pumps, FUEL X-FEED Lever ............... PUMPS ON, X-FEED OFF
AIR COND SHUTOFF Switch..........................................................AUTO
TRI .........................................................................................................GA
- - - - - LANDING CHECKLIST - - - - -Gear.....................................................C+F ...................DOWN, 3 GREEN
Ignition ............................................................................ BOTH / CONTIN
Spoilers, Autobrake System............... LT OUT & ARM, ARM / DISARM
Flaps, Slats ..........................................C+F ............................... 28.
, LAND
Annunciator Panel, Cabin PA ........................CHECKED, COMPLETED
* * * *
INTENTIONALLY LEFT BLANK
INTENTIONALLY LEFT BLANK
ONE ENGINE INOPERATIVE APPROACH AND LANDING
EXPANDED CHECKLIST
Plan a flaps 28. landing with final approach flown at VREF + 10 for go-around capability. After ENGINE FAILURE/FIRE CHECKLIST is complete, use both throttles together for the remainder of the flight. This facilitates TOGA button actuation for go-around, deployment of thrust reversers after landing, and spoiler lever retraction if rejected landing is made after touchdown with left engine inoperative. 中國(guó)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(cè) 1(27)
