Rated maximum continuous augmented thrust


With respect to turbojet engine type certification, means the approved jet thrust that is developed statically or in flight, in standard atmosphere at a specified altitude, with fluid injection or with the burning of fuel in a separate combustion chamber, within the engine operating limitations established under part 33 of this chapter, and approved for unrestricted periods of use.

Source: 14 CFR 1.1, General definitions.

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Glossary last updated 2026-10-28.