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  5. § 33.90
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14 CFR · Part 33

14 CFR § 33.90

Initial maintenance inspection test.

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Read in Subpart F
Part 33 Contents
  • Subpart A: General
  • Subpart B: Design and Construction; General
  • Subpart C: Design and Construction; Reciprocating Aircraft Engines
  • Subpart D: Block Tests; Reciprocating Aircraft Engines
  • Subpart E: Design and Construction; Turbine Aircraft Engines
  • Subpart F: Block Tests; Turbine Aircraft Engines
  • Subpart G: Special Requirements: Turbine Aircraft Engines
  • Appendix A to Part 33: Instructions for Continued Airworthiness
  • Appendix B to Part 33: Certification Standard Atmospheric Concentrations of Rain and Hail
  • Appendix D to Part 33: Mixed Phase and Ice Crystal Icing Envelope (Deep Convective Clouds)

Each applicant, except an applicant for an engine being type certificated through amendment of an existing type certificate or through supplemental type certification procedures, must complete one of the following tests on an engine that substantially conforms to the type design to establish when the initial maintenance inspection is required:

(a)

An approved engine test that simulates the conditions in which the engine is expected to operate in service, including typical start-stop cycles.

(b)

An approved engine test conducted in accordance with § 33.201 (c) through (f).

Regulations Referenced

14 CFR 33.201

Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.

Primary Source

  • Official Source (14 CFR · Part 33)