ENGINE AND TURBOSUPERCHARGER ROTOR OVERSPEED REQUIREMENTS OF 14 CFR SECTION 33.27

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2011

Publisher

Federal Aviation Administration

1. Purpose
2. Applicability
3. Related Regulations
4. Related Documents
5. Definitions
6. Objectives
7. General
8. Acceptable Means of Compliance
9. Factors to be Considered when Determining
Test Conditions
10. Failure Cases

Gives guidance and acceptable methods, but not the only methods, for demonstrating compliance with the rotor strength (overspeed) requirements of Title 14 of the Code of Federal Regulations (14 CFR) 33.27.

DocumentType	Standard
Pages	9
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 33-2 : 2013	GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES
FAA AC 33.70-1 : 2009	GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS
FAA AC 33-3 : 0	TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES
FAA AC 33.64-1 : 2010	GUIDANCE FOR PRESSURIZED ENGINE STATIC PARTS