14 CFR 35.17
§ 35.17 Materials and manufacturing methods.
United States · 14 CFR — Aeronautics and Space · Status: effective
Cite this
- Citation
- 14 CFR 35.17, § 35.17 Materials and manufacturing methods, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/55164
- Permanent ID
ys:prov:55164@1- SHA-256
73b16924025000a7e386e385aad19a000aa91482db67497ec6ce89e1b8c106d1
The hash is SHA-256 of this version's text, with every run of whitespace collapsed to a single space and the ends trimmed. The ID always leads back here, and checking it says whether the text you cited is still the current version.
Full text
(a) The suitability and durability of materials used in the propeller must:
(1) Be established on the basis of experience, tests, or both.
(2) Account for environmental conditions expected in service.
(b) All materials and manufacturing methods must conform to specifications acceptable to the Administrator.
(c) The design values of properties of materials must be suitably related to the most adverse properties stated in the material specification for applicable conditions expected in service.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.