[Code of Federal Regulations]

[Title 14, Volume 1]

[Revised as of January 1, 2006]

From the U.S. Government Printing Office via GPO Access

[CITE: 14CFR33.79]



[Page 785]

 

                     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]