Overweight Landing - Minimum Landing Distance Required
1.
Compare the minimum landing distance required from the table (corrected for wet runway if applicable) to runway available.
2.
Determine go-around capability by checking the approach climb limiting weight in this section. The approach climb limiting weight is the maximum weight at which the aircraft has go-around capability with one engine inoperative in the approach configuration. At gross weights above the charted value minimum go-around capability is not attainable with an engine out.
3.
Determine if the runway available and go-around capability warrant a landing with the actual flight circumstances.
The minimum landing distances in this table are based on the following:
1.
Clean, dry runway
2.
Flaps 40. , slats extended
3.
Over the threshold at 50 FT and at Vref
4.
30 knot headwind at 50 FT height
5.
Maximum braking (Bendix Brakes No. 2608892.1)
6.
Ground Spoilers deployed
7.
Anti-skid operative
8.
No reverse thrust The distances represent actual distances to stop with no margin.
MINIMUM LANDING DISTANCE REQUIRED IN FEET
Airport Pressure Altitude AIRCRAFT GROSS WEIGHT IN LBS.
110,000 120,000 130,000 140,000 150,000
0 2190 2340 2490 2610 2790
1000 2238 2388 2538 2685 2850
2000 2280 2430 2580 2760 2910
3000 2334 2508 2658 2820 2970
4000 2370 2580 2730 2880 3030
5000 2448 2628 2790 2958 3120
6000 2520 2670 2850 3030 3210
7000 2568 2745 2925 3105 3285
8000 2610 2820 3000 3180 3360
Add 15% to the landing distance if the runway is wet.
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LIST OF EFFECTIVE PAGES
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FAA APPROVED ___________________ DON KLOS Principal Operations Inspector
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本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 2(105)
