14 C.F.R. · Aeronautics and Space
14 C.F.R. § 35.43

Propeller hydraulic components.

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Regulatory Text

14 C.F.R. § 35.43 — Propeller hydraulic components.

§ 35.43 Propeller hydraulic components. 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. [Amdt. 35-8, 73 FR 63349, Oct. 24, 2008]

Source: ecfr.gov · govinfo.gov — public domain Official Source ↗
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14 C.F.R. § 35.43
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The regulatory text of 14 C.F.R. § 35.43 is reproduced from the official Code of Federal Regulations as published by the Office of the Federal Register and the National Archives and Records Administration.
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