§33.62. Stress analysis.
14 C.F.R. § 33.62
A stress analysis must be performed on each turbine engine showing the design safety margin of each turbine engine rotor, spacer, and rotor shaft.
Notes, amendments, and revision history
Amendments
[Amdt. 33-6, 39 FR 35466, Oct. 1, 1974]
Authority
Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.
Source
Source: Docket No. 3025, 29 FR 7453, June 10, 1964, unless otherwise noted.
Amendments
[Amdt. 33-6, 39 FR 35466, Oct. 1, 1974]