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  4. Part 33
  5. § 33.4
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14 CFR · Part 33

14 CFR § 33.4

Instructions for Continued Airworthiness.

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Read in Subpart A
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)

The applicant must prepare Instructions for Continued Airworthiness in accordance with appendix A to this part that are acceptable to the Administrator. The instructions may be incomplete at type certification if a program exists to ensure their completion prior to delivery of the first aircraft with the engine installed, or upon issuance of a standard certificate of airworthiness for the aircraft with the engine installed, whichever occurs later.

Referenced By

Interpretations of This Section (3)

  • Oakley (Piedmont Propulsion Systems), 2015
  • Dawson (PMA-207 NAVAIR), 2014
  • MacLeod (AeronauticalRepairStation), 2012

Documents that cite this section, found in their catalog metadata or text. Listed by date, not by significance.

Regulations Referenced

14 CFR Part 33, Appendix A

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)