[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: 14CFR33.55]



[Page 777]

 

                     TITLE 14--AERONAUTICS AND SPACE

 

CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION

 

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

 

          Subpart D_Block Tests; Reciprocating Aircraft Engines

 

Sec. 33.55  Teardown inspection.



    After completing the endurance test--

    (a) Each engine must be completely disassembled;

    (b) Each component having an adjustment setting and a functioning 

characteristic that can be established independent of installation on 

the engine must retain each setting and functioning characteristic 

within the limits that were established and recorded at the beginning of 

the test; and

    (c) Each engine component must conform to the type design and be 

eligible for incorporation into an engine for continued operation, in 

accordance with information submitted in compliance with Sec. 33.4.



[Amdt. 33-6, 39 FR 35466, Oct. 1, 1974, as amended by Amdt. 33-9, 45 FR 

60181, Sept. 11, 1980]