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Refer to figure or Performance Manual SEP 1 Figure 2.1.
The chart addresses take-off performance for single-engine aeroplanes. Given the following conditions, what is the take-off speed for (1) rotation and (2) at a height of 50 ft?

OAT: ISA +10°C
Pressure altitude: 5000 ft
Aeroplane mass: 3400 lb
Headwind component: 5 kt
Flaps: up
Runway: tarred, level, and dry

  • A

    (1) 65 kt and (2) 75 kt

  • B

    (1) 68 kt and (2) 78 kt

  • C

    (1) 71 kt and (2) 82 kt

  • D

    (1)73 kt and (2) 84 kt

Refer to figure.

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