FAA AC 33-1 : 0
Current
The latest, up-to-date edition.
TURBINE ENGINE FOREIGN OBJECT INGESTION AND ROTOR BLADE CONTAINMENT TYPE CERTIFICATION PROCEDURES
Hardcopy , PDF
English
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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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