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(For this question use CAP 698 Figure 4.5) With regard to the take-off performance of a twin jet aeroplane, why does the take-off performance climb limit graph show a kink at 30° C, pressure altitude 0?
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A. |
The engines are pressure limited at lower temperature, at higher temperatures they are temperature limited
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B. |
At higher temperatures the VMBE determines the climb limit mass
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C. |
At lower temperatures one has to take the danger of icing into account
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D. |
At higher temperatures the flat rated engines determines the climb limit mass
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