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FAA AC 33-3 : 0

Current
Current

The latest, up-to-date edition.

TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES
Available format(s)

Hardcopy , PDF

Language(s)

English

1 PURPOSE
2 CANCELLATION
3 CHANGES
4 REFERENCES REGULATIONS
5 SCOPE
6 ACCEPTABLE MEANS OF COMPLIANCE FOR SUBSTANTIATING
   TURBINE AND COMPRESSOR ROTORS

Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the turbine and compressor rotor substantiation requirements in Federal Aviation Regulations, Part 33.

DocumentType
Standard
Pages
8
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 33.64-1 : 2010 GUIDANCE FOR PRESSURIZED ENGINE STATIC PARTS
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
FAA AC 33.15-1 : 0 MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS
FAA AC 33.15-2 : 2011 MANUFACTURING PROCESSES FOR PREMIUM QUALITY NICKEL ALLOY FOR ENGINE ROTATING PARTS
FAA AC 33.70-2 : 2009 DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS
FAA AC 33.70-1 : 2009 GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS

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