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§35.43. Propeller hydraulic components.

14 C.F.R. § 35.43

Applicants must show by test, validated analysis, or both, that propeller components that contain hydraulic pressure and whose structural failure or leakage from a structural failure could cause a hazardous propeller effect demonstrate structural integrity by:
(a)
A proof pressure test to 1.5 times the maximum operating pressure for one minute without permanent deformation or leakage that would prevent performance of the intended function.
(b)
A burst pressure test to 2.0 times the maximum operating pressure for one minute without failure. Leakage is permitted and seals may be excluded from the test.
Notes, amendments, and revision history

Amendments

[Amdt. 35-8, 73 FR 63349, Oct. 24, 2008]

Authority

Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704.

Source

Source: Docket No. 2095, 29 FR 7458, June 10, 1964, unless otherwise noted.

Amendments

[Amdt. 35-8, 73 FR 63349, Oct. 24, 2008]