FAA AC 33-5 : 0
Current
The latest, up-to-date edition.
TURBINE ENGINE ROTOR BLADE CONTAINMENT/DURABILITY
Hardcopy , PDF
English
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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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