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Refer to figure. You are taking-off with a single engine aeroplane and field l...

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Refer to figure.

You are taking-off with a single engine aeroplane and field length limited take off mass from runway

27 in Vmc, for a straight out departure. Given the following information, what will be the expected

obstacle clearance over the water tank on the extended centerline?

Climb gradient: 8%

TAS: 111 kt

Wind component: 5 kt tailwind

1 NM = 6 080 ft

Height Difference = ((GD × TAS)/GS) × Gradient/100

465 ft

215 ft

515 ft

265 ft

100%

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