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CPL Performance & Operation · Mock exam

COPC.3.1Topic: Climb, cruise and descent performance(clear)
Question 1 of 35
⏱ 150:00
Climb, cruise and descent performanceClimb, cruise and descent performance· medium

An aircraft's published Va is 132 kt at MTOW 3,600 kg. The aircraft is flying at 2,800 kg. The correct Va at 2,800 kg is approximately:

V-n (velocity versus load factor) diagram showing the manoeuvre envelope, the accelerated-stall curve, the positive and negative limit load factors, the corner speed Va, and Vno and Vne.
0/35 answered