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FAA AC 33-1 : 0

Current
Current

The latest, up-to-date edition.

TURBINE ENGINE FOREIGN OBJECT INGESTION AND ROTOR BLADE CONTAINMENT TYPE CERTIFICATION PROCEDURES
Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

1 PURPOSE
2 CANCELLATION
3 CHANGES
4 REFERENCES
5 BACKGROUND
6 SCOPE
7 DESIRABLE ENGINE DESIGN FEATURES
8 CLASSIFICATION OF TYPICAL FOREIGN OBJECTS
9 ACCEPTANCE MEANS OF COMPLIANCE
10 SUBSTANTIATION TESTS
11 SUBSTANTIATION CRITERIA

Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the design and construction requirements of Part 33 of the Federal Aviation Regulations.

DocumentType
Standard
Pages
10
PublisherName
Federal Aviation Administration
Status
Current

MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA

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Hardcopy - English
PDF - English
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