[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: 14CFR33.75]



[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. 33.75  Safety analysis.



    It must be shown by analysis that any probable malfunction or any 

probable single or multiple failure, or any probable improper operation 

of the engine will not cause the engine to--

    (a) Catch fire;

    (b) Burst (release hazardous fragments through the engine case);

    (c) Generate loads greater than those ultimate loads specified in 

Sec. 33.23(a); or

    (d) Lose the capability of being shut down.



[Amdt. 33-6, 39 FR 35467, Oct. 1, 1974, as amended by Amdt. 33-10, 49 FR 

6852, Feb. 23, 1984]