FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 33 > Section 75 - Safety analysis
section 33.74 |
section 33.76
It must be shown by analysis that any probable malfunction or any probable single or multiple failure, or any probable improper operation of the engine will not cause the engine to --
(a) Catch fire;
(b) Burst (release hazardous fragments through the engine case);
(c) Generate loads greater than those ultimate loads specified in § 33.23(a); or
(d) Lose the capability of being shut down.
[Amdt. 33-6, 39 FR 35467, Oct. 1, 1974, as amended by Amdt. 33-10, 49 FR 6852, Feb. 23, 1984]
   
Current page: FARs > Part 33 > Section 75 - Safety analysis
section 33.74 |
section 33.76
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