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Private Pilot Licence
· Mock exam
POPA.2.5
Topic:
Climb, cruise and descent performance
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Question 1 of 3
⏱ 210:00
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General flight planning and performance
Climb, cruise and descent performance
· medium
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The 'service ceiling' of an aeroplane is defined as:
A.
The altitude above which the engine can no longer maintain any useful power output whatsoever
B.
The altitude at which the aircraft can no longer maintain a rate of climb of 100 ft/min at maximum continuous power
C.
Field elevation plus 1,000 ft — the minimum safe circuit altitude at the departure aerodrome
D.
The highest cruise altitude permitted by ATC clearance for the aircraft's registered class
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