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: Docket No. 2095, 29 FR 7458, June 10, 1964, unless otherwise noted.
cite as: 14 CFR 35.16