Regulatory Text
14 C.F.R. § 35.16 — Propeller critical parts.
§ 35.16 Propeller critical parts. The integrity of each propeller critical part identified by the safety analysis required by § 35.15 must be established by: (a) A defined engineering process for ensuring the integrity of the propeller critical part throughout its service life, (b) A defined manufacturing process that identifies the requirements to consistently produce the propeller critical part as required by the engineering process, and (c) A defined service management process that identifies the continued airworthiness requirements of the propeller critical part as required by the engineering process. [Amdt. 35-9, 78 FR 4042, Jan. 18, 2013]
Source: ecfr.gov · govinfo.gov — public domain
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Root-LD v1.0 · boisestandard.org
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BS-CFR14-SEC-B57F1F
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REGULATION / FEDERAL-CFR-SECTION
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boisestandard.org
Citation
14 C.F.R. § 35.16
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CFR — Code of Federal Regulations
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PRIMARY-SOURCE
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The regulatory text of 14 C.F.R. § 35.16 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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