FAA AC 33.83 : 2006
Current
The latest, up-to-date edition.
TURBINE ENGINE VIBRATION TEST
Hardcopy , PDF
English
01-01-2006
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1. PURPOSE
2. CANCELLATION
3. APPLICABILITY
4. DEFINITIONS
5. TEST PREPARATION
6. ENGINE TEST CONDITIONS
7. FLUTTER
8. VIBRATORY STRESSES AND MATERIAL ALLOWABLES
9. RESONANT DWELL
10. FAULT CONDITIONS
11. INSTALLATION COMPATIBILITY
12. INSTRUMENTATION
Provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the vibration test requirements of section 33.83 of Title 14 of the Code of Federal Regulations (14 CFR part 33).
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33.83-1 : 2009 | COMPARATIVE METHOD TO SHOW EQUIVALENT VIBRATORY STRESSES AND HIGH CYCLE FATIGUE CAPABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS |
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