[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: 14CFR33.23]



[Page 771]

 

                     TITLE 14--AERONAUTICS AND SPACE

 

CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION

 

PART 33_AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES--Table of Contents

 

               Subpart B_Design and Construction; General

 

Sec. 33.23  Engine mounting attachments and structure.



    (a) The maximum allowable limit and ultimate loads for engine 

mounting attachments and related engine structure must be specified.

    (b) The engine mounting attachments and related engine structure 

must be able to withstand--

    (1) The specified limit loads without permanent deformation; and

    (2) The specified ultimate loads without failure, but may exhibit 

permanent deformation.



[Amdt. 33-10, 49 FR 6851, Feb. 23, 1984]