14CFR vol1 part35 - 9 pages

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Section 35.3
PART 35 - AIRWORTHINESS
Subpart A - General
35.1 Applicability.
35.2 Propeller configuration.
35.3 Instructions for propeller installation
35.4 Instructions for Continued Airworthiness.
35.5 Propeller ratings and operating limitations.
35.7 Features and characteristics.
Subpart B - Design and Construction
35.11 [Reserved]
35.13 [Reserved]
35.15 Safety analysis.
35.16 Propeller critical parts.
35.17 Materials and manufacturing methods.
35.19 Durability.
35.21 Variable and reversible pitch propellers.
35.22 Feathering propellers.
35.23 Propeller control system.
35.24 Strength.
Subpart C - Tests and Inspections
...
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Section 35.4
14 CFR Ch. I (1-1-19 Edition)
(b) Instructions for operating the
Section 35.4 Instructions for Continued Airworthiness.
Section 35.5 Propeller ratings and operating
(a) Propeller ratings and operating
(b) Propeller ratings and operating
(i) For takeoff.
Section 35.7
(a) The propeller may not have features or characteristics, ...
(b) If a failure occurs during a certification test, the app...
Subpart B - Design and
Section 35.11
Section 35.13
Section 35.15
(a)(1) The applicant must analyze the
(i) The propeller system in a typical
(g) of this section, and estimate the
12:50 Apr 30, 2019
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Section 35.15
(b) If significant doubt exists as to
(c) The primary failures of certain
Section 35.16. These instances must be stated
(d) If reliance is placed on a safety
(e) If the safety analysis depends on
Section 35.4. Additionally, if errors in maintenance of the ...
(f) If applicable, the safety analysis
(g) Unless otherwise approved by the
(i) The development of excessive
(i) An inability to feather the propeller for feathering pro...
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Section 35.16
14 CFR Ch. I (1-1-19 Edition)
2013; Amdt. 35-9A, 78 FR 45052, July 26, 2013]
Section 35.16 Propeller critical parts.
(a) A defined engineering process for
(b) A defined manufacturing process
(c) A defined service management
Section 35.17 Materials and manufacturing
(a) The suitability and durability of
(b) All materials and manufacturing
(c) The design values of properties of
Section 35.19 Durability.
Section 35.21 Variable and reversible pitch
(a) No single failure or malfunction
(b) For propellers incorporating a
Section 35.22
(a) Feathering propellers are intended to feather from all f...
(b) Propeller pitch control systems
(c) Feathering propellers must be designed to be capable of ...
Section 35.23
(a) The propeller control system
...
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Section 35.34
(b) The propeller control system
Section 35.15:
(c) Electronic propeller control system imbedded software mu...
(d) The propeller control system
(e) The propeller control system
Section 35.24
Subpart C - Tests and Inspections
Section 35.31
Section 35.33
(a) Each applicant must furnish test
(b) All automatic controls and safety
(c) Any systems or components that
Section 35.34 Inspections,
(a) Before and after conducting the
(b) During all tests, only servicing
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Section 35.35
14 CFR Ch. I (1-1-19 Edition)
Section 35.35 Centrifugal load tests.
(a), (b) and (c) of this section without
(a) The hub, blade retention system,
(b) Blade features associated with
(c) Components used with or attached
Section 35.36 Bird impact.
Section 35.37
(a) Fatigue limits must be established by tests, or analysis...
(b) The fatigue limits must take into
(c) A fatigue evaluation of the propeller must be conducted ...
81 FR 96700, Dec. 30, 2016]
Section 35.38
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Section 35.41
Section 35.39
(a) or (b) of this section, as applicable,
(a) Fixed-pitch and ground adjustable-pitch propellers must ...
90 percent of the rated rotational speed
(b) Variable-pitch propellers must be
(i) Five hours at takeoff power and
(c) An analysis based on tests of propellers of similar desi...
(b) of this section.
Section 35.40
(a) Manually-controllable propellers.
(b) Governing propellers. Fifteen
(c) Feathering propellers. Fifty cycles of feather and unfea...
(d) Reversible-pitch propellers. Two
(e) An analysis based on tests of propellers of similar desi...
Section 35.41
(a) When the applicant seeks approval of a transient maximum...
(b) When the applicant seeks approval of a transient maximum...
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Section 35.42
14 CFR Ch. I (1-1-19 Edition)
Section 35.42 Components of the propeller
Section 35.43 Propeller
(a) A proof pressure test to 1.5 times
(b) A burst pressure test to 2.0 times
(a) This appendix specifies requirements
(b) The Instructions for Continued Airworthiness for each pr...
(c) The applicant must submit to the FAA
(a) The Instructions for Continued Airworthiness must be in ...
(b) The format of the manual or manuals
(a) Propeller Maintenance Section. (1) Introduction informat...
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(b) Propeller Overhaul Section. (1) Disassembly information ...
PART 36 - NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS C...
Subpart A - General
36.1 Applicability and definitions.
36.2 Requirements as of date of application.
36.3 Compatibility with airworthiness requirements.
36.5 Limitation of part.
36.6 Incorporations by reference.
36.7 Acoustical change: Transport category
36.9 Acoustical change: Propeller-driven
36.11 Acoustical change: Helicopters.
36.13 Acoustical change: Tiltrotor aircraft.
Subpart B - Transport Category Large
36.101 Noise measurement and evaluation.
36.103 Noise limits.
36.105 Flight Manual Statement of Chapter
4 equivalency.
36.106 Flight Manual statement of Chapter
14 noise level equivalency.
Subpart C [Reserved]
Subpart D - Noise Limits for Supersonic
...