The Cla-Val Model 340GF Single Point Pressure Fuel Servicing Adapter is a connection adapter for the delivery of pressurized fuel to military refueling tank trucks, and fueling support vehicles only. The design and construction of the Cla-Val 340GF Adapter conform to MIL-A-25896 and MS24484-5.
Cla-Val 340GF Single Point Pressure Fuel Servicing Adapter
The Cla-Val 340GF is a single-point pressure fueling adapter designed for interface with underwing refueling nozzles and hydrant couplers. It is specified for use in military refueling tank trucks, fueling support vehicles, hydrant systems, fixed aviation fuel pipework, and tank farms. Design and construction comply with MIL-A-25896 Rev. E and MS24484-5 standards.
Functional Role
This adapter provides the mechanical interface between fueling equipment and the single-point bayonet connection. Nominal diameter is 2.5”, with a 2.5” single point bayonet coupling interface. Compatible media include refined petroleum products such as aviation fuel, subject to material compatibility verification.
Operating Temperatures and Conditions
- Fuel temperature: -55 °C to +93 °C
- Ambient temperature: -55 °C to +177 °C
- Inlet: threaded or flanged, depending on variant
- Connection configurations: NPT, ISO 7/1-Rp, ANSI 150 lb flange, TTMA housing options
Construction Materials
Body: investment cast stainless steel 17-4PH per AMS 5355, passivated. Poppet assembly and spider: investment cast aluminum A356T6. Spring: stainless steel 17-7PH per AMS 5763. Fasteners: corrosion-resistant steel per AMS 5737. Sealing: fluorosilicone elastomer bonded to poppet.
Connection Options
Available variants:
- 2.5” NPT threaded
- ISO 7/1-Rp 2½ threaded
- 2”, 2.5”, 3”, 4” ANSI 150 lb flange
- 3” and 4” TTMA mounting
Typical Applications
- Underwing pressure refueling
- Hydrant fueling systems
- Refueling tank trucks
- Fixed aviation fuel pipework
- Fuel support vehicles and tank farms
FAQ
Compatible nozzles:
Interfaces with underwing fueling nozzles and hydrant couplers using MS24484-5 interface.
Selection considerations:
Verify inlet connection type, flange pattern, fuel temperature range, nozzle/coupler compatibility, and compliance with MIL-A-25896 or MS24484-5 requirements.