14 CFR 33.79 - Fuel burning thrust augmentor.
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Each fuel burning thrust augmentor, including the nozzle, must—
(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.
[Amdt. 33-6, 39 FR 35468, Oct. 1, 1974]
Title 14 published on 2014-01-01
no entries appear in the Federal Register after this date.