Description
Aviation Couplings
This range of Aviation Couplings have been designed for both Civil & Military use. However, they are not configured for under-wing refuelling.
All units have the following: A maximum working pressure of 10 bar (150 psi). Working temperature range lies within -38C (-36F) to +60C (+140F) Special low temperature seals are used in cold environments.
According to ISO 45 / MS24484 / NATO STANAG 3105 / British Aerospace Specification 2C14.
All units can also be used as bottom loading or primary points refuelling vehicles.
Size
All units are manufactured to accept the international standard: 2½” the point bayonet, hose end refuelling nozzles, according to: ISO 45 / MS24484 / NATO STANAG 3105 / British Aerospace Specification 2C14.
Materials
The couplings consist of high strength aluminium body also a coupling ring in gunmetal and bayonet flange and inner parts in stainless steel and aluminium. All wet parts in aluminium and stainless steel.
Compatibility
They are compatible with the following: ISO 45, MS24484, NATO STANAG 3105, British Aerospace Specification 2C14
Operational Information:
The Aviation Couplings include a bayonet-type connector and are flanged or threaded to suit installation requirements. Each tank unit contains a safe spring loaded valve seating on a tapered seat. The valve is controlled by the action of coupling and uncoupling the hose unit.
Options
Also available is a Drain Plug, Grounding Connection a Filter Strainer with Sight flow indicator.
Please also check our other Aviation and defence equipment
