NATO Stock Number
4820-00-262-7391
Sold in multiples of
1 EA
DEMIL
NO
Thread Direction
Right-hand all ends
Flow Control Device
Disk
Bonnet Type
Inside screw
Bonnet Attachment Method
Union
Renewable Seat Ring Type
Threaded
Maximum Operating Temp
150.0 degrees fahrenheit 2nd response
Maximum Operating Temp
550.0 degrees fahrenheit 1st response
End Application
Grumman; a10 aircraft
Connection Style
G9 plain, optional en (pipe) all ends
Connection Style
Plain, optional en (pipe) all ends
Valve Operation Method
Manual
Connection Type
Threaded internal pipe all ends
Features Provided
Bonnet packing
Maximum Operating Pressure
200.0 pounds per square inch 1st response
Maximum Operating Pressure
400.0 pounds per square inch 2nd response
Thread Size
0.250 inches all ends
Material
Copper alloy 697 stem
Material
Copper alloy 922 body
Material
Steel comp 430f flow control device
Material
Steel comp 430f seat
Material Specification
Astmcu0202 assn standard single material response body
Material Specification
Astmcu0697 assn standard single material response stem
Material Specification
Astmst0101 assn standard single material response flow control device
Material Specification
Astmst0101 assn standard single material response seat
Media For Which Designed
Steam 1st response
Media For Which Designed
Water-oil-gas 2nd response
Style Designator
Straight thru
Thread Series Designator
Npt all ends