[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2007]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR33.66]

[Page 781]
 
                     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]