FAA AC 33-4 : 0
Current
The latest, up-to-date edition.
DESIGN CONSIDERATIONS CONCERNING THE USE OF TITANIUM IN AIRCRAFT TURBINE ENGINES
Hardcopy , PDF
English
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1 PURPOSE
2 APPLICABLE REGULATIONS
3 REFERENCES
4 BACKGROUND
5 DESIGN CONSIDERATIONS
Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the design requirements of Part 33 to minimize the probability of the occurrence of an internal fire when titanium is used in aircraft turbine engines.
| DocumentType |
Standard
|
| Pages |
4
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| FAA AC 33.17-1 : 2009 | ENGINE FIRE PROTECTION SECTION 33.17 |
| FAA AC 33.15-1 : 0 | MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS |
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