[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2003]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR33.74]

[Page 748]
 
                     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. 33.74  Continued rotation.

    If any of the engine main rotating systems will continue to rotate 
after the engine is shutdown for any reason while in flight, and where 
means to prevent that continued rotation are not provided; then any 
continued rotation during the maximum period of flight, and in the 
flight conditions expected to occur with that engine inoperative, must 
not result in any condition described in Sec. 33.75 (a) through (c).

[Doc. No. 28107, 61 FR 28433, June 4, 1996]