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Federal regulations · Through 2026-08-25 · Newer source version available

14 CFR 33.23: Engine mounting attachments and structure.

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Where this section sits in the code
  1. Title 14—Aeronautics and Space
  2. CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
  3. SUBCHAPTER C—AIRCRAFT
  4. PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES
  5. Subpart B—Design and Construction; General

(a) The maximum allowable limit and ultimate loads for engine mounting attachments and related engine structure must be specified.

(b) The engine mounting attachments and related engine structure must be able to withstand—

(1) The specified limit loads without permanent deformation; and

(2) The specified ultimate loads without failure, but may exhibit permanent deformation.

Collected 2026-08-27T02:24:20Z. Source file · JSON

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