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Helical Compression Spring Seat

Model / MPN: 20021A | NSN: 5340-00-358-3417
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
5340-00-358-3417
Sold in multiples of
5 EA
DEMIL
NO
Countersink Angle In Deg
30.0
Counterbore Diameter
Between 0.5130 inches and 0.5180 inches
Overall Height
0.3860 inches
First Step Diameter
Between 1.1550 inches and 1.1650 inches
Bore Diameter
0.3910 inches
Design Type
Solid
Countersink Diameter
Between 0.9330 inches and 0.9380 inches
End Diameter
Between 0.8960 inches and 0.9060 inches
Distance From End To First Step
0.2920 inches
Counterbore Length
0.2820 inches
Features Provided
Casehardened
Material
Steel, aisi b1113 or steel sae 1113
Material
Steel, aisi b1113 or steel sae 1113
Fsc Application Data
Engine, gasoline, nonaircraft

Pricing and Availability

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20021A Cross Reference
  • R683
  • 20021A