[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: 14CFR33.65]



[Page 778]

 

                     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. 33.65  Surge and stall characteristics.



    When the engine is operated in accordance with operating 

instructions required by Sec. 33.5(b), starting, a change of power or 

thrust, power or thrust augmentation, limiting inlet air distortion, or 

inlet air temperature may not cause surge or stall to the extent that 

flameout, structural failure, overtemperature, or failure of the engine 

to recover power or thrust will occur at any point in the operating 

envelope.



[Amdt. 33-6, 39 FR 35466, Oct. 1, 1974]