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FAA AC 33.14-1 : 0

FAA AC 33.14-1 : 0

Current

Current

The latest, up-to-date edition.

DAMAGE TOLERANCE FOR HIGH ENERGY TURBINE ENGINE ROTORS

Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

1 PURPOSE
2 RELATED READING MATERIAL
3 DEFINITIONS
4 BACKGROUND
5 APPLICABILITY

Explains an acceptable means for showing compliance with the requirements of Section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requirements applicable to the design and life management of high energy rotating parts of aircraft gas turbine engines.

DocumentType
Standard
Pages
128
PublisherName
Federal Aviation Administration
Status
Current

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

SAE AIR 1537 : 1996 REPORT ON AIRCRAFT ENGINE CONTAINMENT
SAE AIR 4003 : 1991 REPORT ON AIRCRAFT ENGINE CONTAINMENT

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Hardcopy - English
PDF - English
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