Volume: 1Date: 2023-01-01Original Date: 2023-01-01Title: Section 33.79 - Fuel burning thrust augmentor.Context:
Title 14 - Aeronautics and Space. CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION. SUBCHAPTER C - AIRCRAFT. PART 33 - AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES. Subpart E - Design and Construction; Turbine Aircraft Engines.
§ 33.79Fuel burning thrust augmentor.Each fuel burning thrust augmentor, including the nozzle, must—(a) Provide cutoff of the fuel burning thrust augmentor;(b) Permit on-off cycling;(c) Be controllable within the intended range of operation;(d) Upon a failure or malfunction of augmentor combustion, not cause the engine to lose thrust other than that provided by the augmentor; and
(e) Have controls that function compatibly with the other engine controls and automatically shut off augmentor fuel flow if the engine rotor speed drops below the minimum rotational speed at
which the augmentor is intended to function.
Code of Federal Regulations /
Title 14 - Aeronautics and Space /
Vol. 1 / 2023-01-01726