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

14 CFR 33.55: Teardown inspection.

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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 D—Block Tests; Reciprocating Aircraft Engines

After completing the endurance test—

(a) Each engine must be completely disassembled;

(b) Each component having an adjustment setting and a functioning characteristic that can be established independent of installation on the engine must retain each setting and functioning characteristic within the limits that were established and recorded at the beginning of the test; and

(c) Each engine component must conform to the type design and be eligible for incorporation into an engine for continued operation, in accordance with information submitted in compliance with § 33.4.

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

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