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Helical Compression Spring Seat

Model / MPN: AS87209 | NSN: 5340-00-118-2346
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
5340-00-118-2346
Sold in multiples of
DEMIL
NO
Overall Height
Between 0.5320 inches and 0.5420 inches
First Step Diameter
Between 1.6870 inches and 1.6970 inches
First Step Length
0.1090 inches
Second Step Diameter
2.0000 inches
Bore Diameter
Between 0.9440 inches and 0.9470 inches
Material Hardness Rating
Between 35.0 rockwell c and 40.0 rockwell c
Design Type
Solid
End Diameter
Between 1.2450 inches and 1.2550 inches
Distance From End To First Step
0.3030 inches
Material
Steel, ams 6415
Material
Steel comp 4340
Material Specification
Ams 6415 assn standard single material response
Style Designator
Seat
Fsc Application Data
Aircraft eng r1830

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AS87209 Cross Reference
  • 20167
  • 87209
  • 87209
  • 20167