FAA AC 35-1 : 2008
Current
The latest, up-to-date edition.
CERTIFICATION OF PROPELLERS
Hardcopy , PDF
English
01-01-2008
CHAPTER 1 - INTRODUCTION
1.1 General
1.2 Definitions
CHAPTER 2 - GENERAL
2.1 Propeller System and Propeller Type Design
2.2 Components Approved for Use with the Propeller
2.3 De-Icing Equipment
2.4 Propeller-Level Failure Conditions
2.5 Hazardous Propeller Effects
2.6 Major Propeller Effects
CHAPTER 3 - GUIDANCE FOR SUBPART A - GENERAL
3.1 Section 35.1 Applicability
3.2 Section 35.2 Propeller Configuration
3.3 Section 35.3 Instructions for Propeller Installation
and Operation
3.4 Section 35.4 Instructions for Continued Airworthiness
3.5 Section 35.5 Propeller Ratings and Operating Limitations
3.6 Section 35.7 Features and Characteristics
CHAPTER 4 - GUIDANCE FOR SUBPART B - DESIGN AND CONSTRUCTION
4.1 Section 35.15 Safety Analysis
4.2 Section 35.17 Materials and Manufacturing Methods
4.3 Section 35.19 Durability
4.4 Section 35.21 Variable and Reversible Pitch Propellers
4.5 Section 35.22 Feathering Propellers
4.6 Section 35.23 Propeller Control System
4.7 Section 35.24 Strength
CHAPTER 5 - GUIDANCE FOR SUBPART C - TYPE SUBSTANTIATION
5.1 Section 35.33 General
5.2 Section 35.34 Inspections, Adjustments and Repairs
5.3 Section 35.35 Centrifugal Load Tests
5.4 Section 35.36 Bird Impact
5.5 Section 35.37 Fatigue Limits and Evaluation
5.6 Section 35.38 Lightning Strike
5.7 Section 35.39 Endurance Test
5.8 Section 35.40 Functional Test
5.9 Section 35.41 Overspeed and Overtorque
5.10 Section 35.42 Components of the Propeller Control System
5.11 Section 35.43 Propeller Hydraulic Components
Describes guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with provisions of the requirements of part 35 of Title 14 of the Code of Federal Regulations (14 CFR part 35).
DocumentType |
Standard
|
Pages |
28
|
PublisherName |
Federal Aviation Administration
|
Status |
Current
|
FAA AC 20-66 : 2011 | PROPELLER VIBRATION AND FATIGUE |
FAA 8110.4 : 2011 | TYPE CERTIFICATION |
FAA AC 35.37-1 : 2011 | PROPELLER FATIGUE LIMITS AND EVALUATION |
FAA AC 20-66 : 2011 | PROPELLER VIBRATION AND FATIGUE |
FAA AC 20-107 : 2009 | COMPOSITE AIRCRAFT STRUCTURE |
FAA AC 35.4-1 : 0 | PROPELLER INSTRUCTIONS FOR CONTINUED AIRWORTHINESS |
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