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Helical Compression Spring Seat

Model / MPN: 63800 | NSN: 5340-00-384-1024
ITAR Registered seal

A circular item, usually having a flat or grooved flange, bos (es), and/or counterbore designed to accommodate the end of the spring. It is used to position the spring, but does not encase the spring or restrain lateral motion. It may be used in conjunction with a retainer, helical compression spring. Excludes washer (1), (as modified) ; seat, ball socket and holder, spring. See also rotor, engine poppet valve.

Product Details
NATO Stock Number
5340-00-384-1024
Sold in multiples of
1 EA
DEMIL
NO
Chamfer Angle In Deg
30.0
Overall Height
0.5620 inches
First Step Diameter
Between 1.4275 inches and 1.4375 inches
First Step Length
0.0940 inches
Second Step Diameter
1.8120 inches
Bore Diameter
Between 0.7480 inches and 0.7510 inches
Seat Angle In Deg
13.0
Second End Diameter
0.8750 inches
Design Type
Solid
End Diameter
0.8120 inches
Bore Taper In Deg
8.583
Distance From End To First Step
0.2810 inches
Features Provided
Casehardened
Material
Steel, aisi 81112 or steel, sae 1112
Material
Steel, aisi 81112 or steel, sae 1112
Fsc Application Data
1. Valve assemblies, gasoline engine, except aircraft prime moving and starting engine types

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63800 Cross Reference
  • 1A63800
  • 3H1926-1R21
  • 05-51584