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  5. § 33.45
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14 CFR · Part 33

14 CFR § 33.45

Calibration tests.

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Read in Subpart D
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)
(a)

Each engine must be subjected to the calibration tests necessary to establish its power characteristics and the conditions for the endurance test specified in § 33.49. The results of the power characteristics calibration tests form the basis for establishing the characteristics of the engine over its entire operating range of crankshaft rotational speeds, manifold pressures, fuel/air mixture settings, and altitudes. Power ratings are based upon standard atmospheric conditions with only those accessories installed which are essential for engine functioning.

(b)

A power check at sea level conditions must be accomplished on the endurance test engine after the endurance test. Any change in power characteristics which occurs during the endurance test must be determined. Measurements taken during the final portion of the endurance test may be used in showing compliance with the requirements of this paragraph.

Regulations Referenced

14 CFR 33.49

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)