[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: 14CFR33.66]



[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. 33.66  Bleed air system.



    The engine must supply bleed air without adverse effect on the 

engine, excluding reduced thrust or power output, at all conditions up 

to the discharge flow conditions established as a limitation under Sec. 

33.7(c)(11). If bleed air used for engine anti-icing can be controlled, 

provision must be made for a means to indicate the functioning of the 

engine ice protection system.



[Amdt. 33-10, 49 FR 6851, Feb. 23, 1984]