80 - ATPL - Given that the characteristics of a three engine turbojet aeroplane are as follows: Thrust = 50000 Newton / Engine. g = 10 m/s². Drag = 72569 N. Minimum steady gradient of climb (2nd segment) = 2.7%. SIN (Angle of climb) = (Thrust - Drag) / Weight. The maximum take-off mass under 2nd segment conditions with 1 engine out is:
Question 80 - Performance - ATPL - Airline Transport Pilot license
101596 kg
209064 kg
74064 kg
286781 kg
Training tests and timed exam simulations ATPL - Airline Transport Pilot license
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