[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: 14CFR33.74]



[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. 33.74  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]