AVIA305. 3
Liberty University
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LU AVIA 305 Test 3 answered
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--19May 20222020/2021A+
- LU AVIA 305 Test 3 
•	Question 1 
2.5 out of 2.5 points 
Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift - Angle of Attack (AOA) curves. 
For a safe takeoff, the Critical Field Length must be no greater than the runway available 
An increase in density altitude has what effect on takeoff performance
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