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Aircraft Performance

Aircraft Performance. DA = 3000’. DA = 8000’. PA = 4750’. PA = 4750’. TEMP = -8 F TEMP = +18 C. TEMP = 98. PA = 6000’. PA = 6000’. PA =1000’. Outside air temperature 20 C. ROC = 650 fpm. Rate of climb = 375 fpm. Outside air temperature -20 C. Rate of climb = 580 fpm.

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Aircraft Performance

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  1. Aircraft Performance

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

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

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

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