NATO Stock Number
2810-00-210-5812
Sold in multiples of
1 EA
DEMIL
NO
End Application
Aircraft eng r2800
General Description
Matl steel per ams 6260; case hardness per rockwell a79 min and a85 max; core hardness per rockwell c30 min and c40 max; body od 8.182 in. Min and 8.184 in. Max; length 1.570 in.; flange od 9.880 in.; flange has 12 holes of diameter 0.625 in., 16 holes of diameter 0.516 in., and 1 hole of diameter 0.3437 in.