FAA-AC-33.83-1
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- 197 Downloads
- 281.96 KB File Size
- 1 File Count
- May 26, 2016 Create Date
- May 26, 2016 Last Updated
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Comparative Method to Show Equivalent Vibratory Stresses and High Cycle Fatigue Capability for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit
| File | Action |
|---|---|
| FAA-AC-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.pdf | Download |
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