§35.16. Propeller critical parts.
14 C.F.R. § 35.16
The integrity of each propeller critical part identified by the safety analysis required by § 35.15 must be established by:
A defined engineering process for ensuring the integrity of the propeller critical part throughout its service life,
A defined manufacturing process that identifies the requirements to consistently produce the propeller critical part as required by the engineering process, and
A defined service management process that identifies the continued airworthiness requirements of the propeller critical part as required by the engineering process.
Notes, amendments, and revision history
Amendments
[Amdt. 35-9, 78 FR 4042, Jan. 18, 2013]
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. 35-9, 78 FR 4042, Jan. 18, 2013]