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FAA Federal Aviation Regulations (FARS, 14 CFR)

FARs   >   Part 33   >   Section 62 - Stress analysis

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A stress analysis must be performed on each turbine engine showing the design safety margin of each turbine engine rotor, spacer, and rotor shaft.

[Amdt. 33-6, 39 FR 35466, Oct. 1, 1974]

 

 

 

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