[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: 14CFR33.65]

[Page 769]
 
                     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]