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Higher seat back angle (>60°) will result in __________(a) improvement to withstand high- g loads(b) drag increment(c) outside vision improvement(d) maximum dragThis question was posed to me during an interview for a job.The doubt is from Crew Station in chapter Crew Station, Passengers, and Payload of Aircraft Design

Answer»

The CORRECT choice is (a) improvement to withstand high- g loads

To explain I would say: Typically, seat back ANGLE can vary from 12° to 40°. However, some more advanced studies consider seat back angle of up to 70-75 degrees. This is much HIGHER seat back angle will improve pilot’s ABILITY to withstand high g turns.



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