[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: 14CFR35.1]



[Page 807-808]

 

                     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 808]]





    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 cer tif i cates, 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]