This aerospace specification defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure.
| SAE International | |
|---|---|
| Product Category | Standards and Technical Documents |
| Product Number | AS1650A |
| Product Name | Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification |
