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Aircraft Performance. TEMP = 98 PA = 4750’ DA = 8000’ DA = 3000’ PA = 4750’ TEMP = -8 F TEMP = +18 C.

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Presentation on theme: "Aircraft Performance. TEMP = 98 PA = 4750’ DA = 8000’ DA = 3000’ PA = 4750’ TEMP = -8 F TEMP = +18 C."— Presentation transcript:

1 Aircraft Performance

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4 TEMP = 98 PA = 4750’ DA = 8000’ DA = 3000’ PA = 4750’ TEMP = -8 F TEMP = +18 C

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7 Outside air temperature 20 C PA = 6000’ Rate of climb = 375 fpm Outside air temperature -20 C PA = 6000’ Rate of climb = 580 fpm PA =1000’ ROC = 650 fpm

8 Take Off Distance Chart Verify that you match the conditions in the landing chart Find the row and column for the temperature and pressure altitude. pressure altitude Read the ground roll and distance to clear a 50 foot object. Interpolate for intermediate values as necessary.Interpolate Apply necessary correction factors: Wind Grass runway Wind Grass runway

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