| Number | Title | Status | Office | Date |
|---|---|---|---|---|
| 33.14-1 |
Damage Tolerance for High Energy Turbine Engine Rotors - Including Change 1
This advisory circular describes an acceptable means for showing compliance with the requirements of section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). |
Active | ANE-110 | 2001-01-08 |
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