NATO Stock Number
2915-00-024-6014
Sold in multiples of
1 EA
DEMIL
DEMIL/MLI
End Application
J57 aircraft engine
General Description
Steel, aisi 302 or 303; 0.320 in. Min, 0.330 in. Max thk, 0.682 in. Min, 0.685 in. Max dia; groove 0.14 in. W, 0.508 in. Min, 0.517 in. Max dia; flange one side 0.03 in. Thk, 0.738 in. Min, 0.740 in. Max dia; center hole 0.18-0.22 in. Dp, 0.28-0.31 in. Dia, tap .250-28nf-2, dp .12 min full thd; part of surge and temp limiting valve assembly for main fuel control, jfc 8