EASA ATPL Package (former JAA) Performance

Performance Turbine Engines

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Question 7159
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A four jet-engine aeroplane (mass = 150 000 kg) is established on climb with all engines operating. The lift-to-drag ratio is 14. Each engine has a thrust of 75 000 Newton. The gradient of climb is: (given: g= 10 m/s²)

A
27%.
B
12.86%.
C
1.286%.
D
7.86%.