| Number | Title | Status | Office | Date |
|---|---|---|---|---|
| 33.83-1 |
Comparative Method to Show Equivalent Vibratory Stresses and High Cycle Fatigue Capability for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts
This advisory circular (AC) describes a comparative test and analysis method that may be used for turbine engine or auxiliary power unit (APU) blades or vanes when produced under parts manufacturer approval (PMA). |
Active | ANE-111 | 2009-09-08 |
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