DESIGN CONSIDERATIONS CONCERNING THE USE OF TITANIUM IN AIRCRAFT TURBINE ENGINES

Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

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