-217/-217A
Automatic Ground Spoilers Actuator Inop - Takeoff Weight Corr. (lbs.)
Runway slopes -2% to +1.7% / Winds -10 to +30
Airport Pressure Altitude Runway Length 6000 7000 8000 9000 10,000 11,000 12,000 13,000
Sea Flaps 4.
Level 5100 4500 3900 3400 3100 2800 2600 2300
2000 4900 4300 3900 3400 3100 2800 2500 2400
4000 N/A 4100 3700 3300 3100 2800 2500 2400
6000 N/A 3700 3400 3100 2900 2700 2400 2200
Sea Flaps 11.
Level 5300 4700 4000 3600 3200 2900 2600 2300
2000 5200 4600 4000 3500 3200 2800 2600 2400
4000 4900 4400 3900 3400 3100 2800 2600 2300
6000 4400 4000 3600 3200 3000 2600 2500 2300
Sea Flaps 15.
Level 5200 4700 4300 3700 3300 2900 2800 2500
2000 5000 4500 4200 3800 3400 3100 2800 2400
4000 4800 4400 4100 3800 3400 3100 3200 2600
6000 4400 4200 3900 3800 3400 3100 2800 2900
Example: The sample problem on page 9 calculated a Runway Limit gross weight of 155,300 lbs. If the automatic ground spoilers actuator was inoperative, the takeoff weight penalty for a flaps 11. takeoff on runway 8 is 3600 lbs. (Interpolation between 3200 and 3600 is authorized if necessary.) The corrected Runway Limit Gross weight is 151,700 and the Climb Limit gross weight remains 149,500 yielding a maximum allowable takeoff weight of 149,500 lbs.
Inboard Ground Spoilers Inoperative
If the Flight Crew uses the Runway Analysis in the Flight Departure Paperwork to determine takeoff capability, the appropriate takeoff weight correction from the table below should be subtracted from the maximum runway limit weight.
-217/-217A
Inboard Ground Spoilers Inoperative - Takeoff Weight Corr. (lbs.)
Runway slopes -2% to +1.7% / Winds -10 to +30 / A/C On or Off
Airport Pressure Altitude Runway Length 6000 7000 8000 9000 10,000 11,000 12,000 13,000
Sea Flaps 4.
Level 3100 2800 2400 2200 1900 1800 1600 1400
2000 3000 2700 2400 2100 1900 1800 1600 1500
4000 2800 2500 2300 2100 1900 1700 1600 1500
6000 2600 2300 2100 1900 1800 1600 1500 1300
Sea Flaps 11.
Level 3300 2900 2500 2200 2000 1800 1600 1400
2000 3200 2800 2500 2200 2000 1800 1600 1500
4000 3000 2700 2400 2100 1900 1800 1600 1500
6000 2700 2500 2300 2000 1900 1600 1500 1500
Sea Flaps 15.
Level 3300 2900 2700 2300 2200 1900 1700 1600
2000 3100 2800 2600 2400 2300 2000 1600 1700
4000 3000 2700 2600 2400 2200 2000 1700 1600
6000 2700 2600 2400 2400 2200 1900 1900 1600
Example: The sample problem on page 9 calculated a Runway Limit gross weight of 155,300 lbs. If the inboard ground spoilers were inoperative, the takeoff weight penalty for a flaps 11. takeoff on runway 8 is 2200 lbs. (Interpolation between 2200 and 2000 is authorized if necessary.) The corrected Runway Limit Gross weight is 153,100 and the Climb Limit gross weight remains 149,500 yielding a maximum allowable takeoff weight of 149,500 lbs.
Right Engine Hydraulic Pump Inoperative
If the Flight Crew uses the Runway Analysis in the Flight Departure Paperwork to determine takeoff capability, the appropriate takeoff weight correction from the table below should be subtracted from the maximum runway limit weight.
-217/-217A
Right Engine Hydraulic Pump Inop - Takeoff Weight Correction (lbs.)
Runway slopes -2.0% to +1.7% / Winds -10 to +30 / A/C on or off
Airport Pressure Altitude Runway Length 6000 7000 8000 9000 10,000 11,000 12,000 13,000
SL to Flaps 4.
1000 N/A 1700 1500 1300 1200 1100 1000 900
2000 N/A 1600 1400 1300 1200 1000 1000 900
4000 N/A 1500 1400 1200 1100 1000 1000 900
6000 N/A 1400 1300 1200 1100 1000 900 900
SL to Flaps 11.
1000 N/A 1700 1500 1300 1200 1100 0 0
2000 N/A 1600 1400 1300 1100 1000 0 0
4000 N/A 1500 1400 1200 1100 1000 0 0
6000 N/A 1500 1300 1200 1100 900 0 0
SL to Flaps 15.
1000 N/A 1700 1600 1400 1300 1200 0 0
2000 N/A 1600 1500 1300 1200 1100 0 0
4000 N/A 1600 1400 1300 1200 1100 0 0
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本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 2(80)
