[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: 14CFR35.35]

[Page 800]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 35--AIRWORTHINESS STANDARDS: PROPELLERS--Table of Contents
 
                    Subpart C--Tests and Inspections
 
Sec. 35.35  Blade retention test.

    The hub and blade retention arrangement of propellers with 
detachable blades must be subjected to a centrifugal load of twice the 
maximum centrifugal force to which the propeller would be subjected 
during operations within the limitations established for the propeller. 
This may be done by either a whirl test or a static pull test.

(Secs. 313(a), 601, and 603, 72 Stat. 752, 775, 49 U.S.C. 1354(a), 1421, 
and 1423; sec. 6(c), 49 U.S.C. 1655(c))

[Amdt. 35-4, 42 FR 15047, Mar. 17, 1977]