An aircraft is flying at TAS of 1100 kt and FL650. A change of 0.1 mach causes a change in TAS of 57 kt. The temperature deviation at FL650 assuming an ISA atmosphere is:
a) +6
b) +3
c) -3
d) -6
An aircraft is flying at TAS of 1100 kt and FL650. A change of 0.1 mach causes a change in TAS of 57 kt. The temperature deviation at FL650 assuming an ISA atmosphere is:
a) +6
b) +3
c) -3
d) -6
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