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JAA ATPL Question 5037
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JAA ATPL Question 5037
Schiphol, Netherlands
@sachinp
(g)atpl-question-bank
Question
21 Oct 2020
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the thrust and the maximum thrust.
the thermal power of fuel-flow and shaft power.
usable (power available) power of the propeller and shaft power.
the usable (power available) power and the maximum power.
2,025 votes ยท 22 hours left
Propeller efficiency may be defined as the ratio between:
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