GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2009

Publisher

Federal Aviation Administration

1. PURPOSE
2. APPLICABILITY
3. RELATED REGULATIONS
4. RELATED GUIDANCE
5. DEFINITIONS
6. INTRODUCTION
7. GENERAL
8. GUIDANCE FOR DEFINING AN ENGINEERING PLAN
9. GUIDANCE FOR DEFINING A MANUFACTURING PLAN
10. GUIDANCE FOR DEFINING A SERVICE MANAGEMENT PLAN
11. AIRWORTHINESS LIMITATION SECTION

Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of section 33.70 of Title 14 of the Code of Federal Regulations (14 CFR part 33).

DocumentType	Standard
Pages	23
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 33.27-1 : 2011	ENGINE AND TURBOSUPERCHARGER ROTOR OVERSPEED REQUIREMENTS OF 14 CFR SECTION 33.27
FAA AC 33.70-2 : 2009	DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS

FAA AC 33.4-2 : 0	INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY
FAA AC 33-3 : 0	TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES
FAA AC 33.4-1 : 0	INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
FAA AC 33.14-1 : 0	DAMAGE TOLERANCE FOR HIGH ENERGY TURBINE ENGINE ROTORS

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FAA AC 33.70-1 : 2009

GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS

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Abstract

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Standards Referenced By This Book

Standards Referencing This Book

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