Summary
This ARP applies to turbine engines that are to be used in helicopters. It provides the engine designer guide lines in achieving a satisfactory turbine engine drive shaft connection.
Notes
Approuvée 1989-05-01, 1989-05-00.
Technical characteristics
| Publisher | SAE International |
| Publication Date | 01/20/2023 |
| Confirmation Date | 01/20/2023 |
| Page Count | 3 |
| Themes | Aerospace |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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