[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2004]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR33.75]

[Page 772]
 
                     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]