[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2004]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR33.79]

[Page 776]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 33--AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES--Table of Contents
 
      Subpart E--Design and Construction; Turbine Aircraft Engines
 
Sec. 33.79  Fuel 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.

[Amdt. 33-6, 39 FR 35468, Oct. 1, 1974]

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