A) The takeoff distance required will be greater than that calculated for standard conditions because of the combined effect of high pressure altitude and high temperature. B) The takeoff distance required will be less than that calculated for standard conditions because the low QNH increases engine thrust. C) The takeoff distance required remains unchanged because mass is the only factor affecting takeoff performance. D) The takeoff distance required will be reduced due to the high temperature reducing air density and thus reducing drag.
Elias blinked. "What?"
"Navigation." Elias grimaced. "I hate the compass turns." atpl exam question bank
"Getting existential over the RAT, Elias?" A) The takeoff distance required will be greater
