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What was the maximum temperature that aluminum could sustain over the life of the aircraft?

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What was the maximum temperature that aluminum could sustain over the life of the aircraft?

(a) 1000 ℃

(b) 1270 ℃

(c) 100 ℃

(d) 127 ℃

I have been asked this question in my homework.

Origin of the question is Aircraft Systems and Aviation in chapter Aircraft Systems and Aviation Overview of Aircraft Maintenance

1 Answer

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Correct option is (d) 127 ℃

Easiest explanation: Aluminium material could sustain a maximum temperature of about 127 ℃ (Approximately 261 ℉) over the complete life of the aircraft. Such temperature limitations in turn decreased the top speed of the aircraft.

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