Serving our customers with quality and safety first.
grooved w/external locking flange
0.040in.
0.040in.
1.775in. and 1.780in. ⁓1-25/32"
2.4268in. and 2.4273in.
1.3380in. and 1.3385in.
0.621in.
25.0 microinches inside
25.0 microinches right face
60.0 microinches outside
offcenter boss on bottom 1.950 in. od, 0.561 in. h w/4 holes 0.195 in. dia, 0.48 in. dp on end; body w/6 holes 0.195 in. dia, 0 476 in. dp on end, 1 hole thru 0.156 in. dia; side flatted 1.051 in. FACE-TO-Cen
F110-GE-100 acft eng fuel pump
1EA
Schedule B number: 8411917050
nmfc 128000
Parts of turbojet and turbopropeller aircraft engines, other than for use in civil aircraft
FSC 2935 ⁓ Engine system cooling components, aircraft prime moving
Note-this class includes only cooling system components for aircraft and/or guided missile prime movers only.
Excluding cooling system components not specifically designed for use with aircraft engines.
offcenter boss on bottom 1.950 in. od, 0.561 in. h w/4 holes 0.195 in. dia, 0.48 in. dp on end; body w/6 holes 0.195 in. dia, 0 476 in. dp on end, 1 hole thru 0.156 in. dia; side flatted 1.051 in. face-to-cen 1.775" overall length
Nothing similar to this part number was found in our inventory
A cylindrical item with or without flange(s), designed to be inserted in a pump casing or secured to the impeller of a centrifugal pump. it is used for the purpose of providing a close running clearance between the impeller and casing in order to prevent or overcome leakage due to erosion. it may also be used as a diffuser ring in the suction and discharge throats of valves.