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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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 1989-05-01 |
| ICS | 49.050 : Aerospace engines and propulsion systems
|
| Number of pages | 3 |
| Set | AEROPAKS10U-10 |
| Year | 1980 |
| Document history | |
| Country | USA |
| Keyword | SAE 721;SAE ARP721;SAE ARP721;SAE ARP 721 |