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FAA AC 33-5 : 0

Current
Current

The latest, up-to-date edition.

TURBINE ENGINE ROTOR BLADE CONTAINMENT/DURABILITY
Available format(s)

Hardcopy , PDF

Language(s)

English

1 PURPOSE
2 RELATED FAR
3 RELATED READING MATERIAL
4 BACKGROUND
5 DEFINITIONS
6 DISCUSSION

Gives guidance and acceptable methods, but not the only methods, that may be used by an acceptable in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the Federal Aviation Regulations (FAR).

DocumentType
Standard
Pages
8
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 43-207 : 2002 CORRELATION, OPERATION, DESIGN, AND MODIFICATION OF TURBOFAN/JET ENGINE TEST CELLS
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA

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£16.70
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