Steel b50tf39 cl-a; 1.215 in. Min, 1.235 in. Max lg; 0.230 in. Min, 0.250 in. Max w; 0.062 in. Min, 0.072 in. Max diameter through 3 holes
A single or multi-piece item of metallic construction, specifically designed to form either a tight fuel or oil seal in an engine, gas turbine, aircraft.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6320-00-674-1361
NSN 5920-01-654-4440
NSN 6145-00-264-2137
NSN 5965-01-434-4095
NSN 6220-01-573-6204
NSN 5960-01-182-3676
NSN 6135-01-377-5729
NSN 5960-01-414-1677
NSN 6150-00-994-2622
NSN 5950-01-535-6326
NSN 2925-01-432-8452
NSN 5915-00-025-1763