FAA AC 33.14-1 : 0
Current
The latest, up-to-date edition.
DAMAGE TOLERANCE FOR HIGH ENERGY TURBINE ENGINE ROTORS
Hardcopy , PDF
English
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1 PURPOSE
2 RELATED READING MATERIAL
3 DEFINITIONS
4 BACKGROUND
5 APPLICABILITY
Explains an acceptable means for showing compliance with the requirements of Section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requirements applicable to the design and life management of high energy rotating parts of aircraft gas turbine engines.
| DocumentType |
Standard
|
| Pages |
128
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33.70-2 : 2009 | DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS |
| FAA AC 33.70-1 : 2009 | GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS |
| SAE AIR1537A | REPORT ON AIRCRAFT ENGINE CONTAINMENT |
| SAE AIR 4003 : 1991 | REPORT ON AIRCRAFT ENGINE CONTAINMENT |
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