[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2007]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR35.1]

[Page 810-811]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 35_AIRWORTHINESS STANDARDS: PROPELLERS--Table of Contents
 
                            Subpart A_General
 
Sec.  35.1  Applicability.




                            Subpart A_General

Sec.  
35.1 Applicability.
35.3 Instruction manual for installing and operating the propeller.
35.4 Instructions for Continued Airworthiness.
35.5 Propeller operating limitations.

                    Subpart B_Design and Construction

35.11 Applicability.
35.13 General.
35.15 Design features.
35.17 Materials.
35.19 Durability.
35.21 Reversible propellers.
35.23 Pitch control and indication.

                     Subpart C_Tests and Inspections

35.31 Applicability.
35.33 General.
35.35 Blade retention test.
35.37 Fatigue limit tests.
35.39 Endurance test.
35.41 Functional test.
35.42 Blade pitch control system component test.
35.43 Special tests.
35.45 Teardown inspection.
35.47 Propeller adjustments and parts replacements.

Appendix A to Part 35--Instructions for Continued Airworthiness

    Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704.

[[Page 811]]


    Source: Docket No. 2095, 29 FR 7458, June 10, 1964, unless otherwise 
noted.



    (a) This part prescribes airworthiness standards for the issue of 
type certificates and changes to those certificates, for propellers.
    (b) Each person who applies under Part 21 for such a certificate or 
change must show compliance with the applicable requirements of this 
part.

[Amdt. 35-3, 41 FR 55475, Dec. 20, 1976]