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SAE AS 5830A:2017-05-16
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement SpecificationMore info
This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing and components in aircraft fuel, vent and other systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for the service life of the aircraft system. The assembled coupling is for use from -65 to +200 °F at nominal operating pressures (125 psig for -08 through -64 and 30 psig for -72 through -88).
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.050 : Aerospace engines and propulsion systems |
| Number of pages | 34 |
| Replace | SAE AS 5830:2013-01-09 |
| Set | AEROPAKS10U-10 |
| Year | 2017 |
| Document history | SAE AS 5830:2013-01-09 |
| Country | USA |
| Keyword | SAE 5830;SAE AS5830A;SAE AS5830A;SAE AS 5830 |