(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? A. The engines are pressure limited at lower temperature, at higher temperatures they are temperature limited B. At higher temperatures the VMBE determines the climb limit mass C. At lower temperatures one has to take the danger of icing into account D. At higher temperatures the flat rated engines determines the climb limit mass

 

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