Ring, mating, seal, t.O. 2j-f110-14; 8.300 in. Id; 0.100 in. Dia. 16 holes eq sp; o.266 in. Dia. 15 holes, 20 slot eq sp; case is located on the endof the turbine rotor assembly
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 6150-01-029-5329
NSN 5965-00-083-8157
NSN 5990-00-424-8872
NSN 5905-01-460-7739
NSN 5920-01-063-6499
NSN 5905-00-469-3482
NSN 4140-01-025-8487
NSN 5925-00-436-3454
NSN 5935-01-612-0611
NSN 5925-01-129-9074
NSN 5895-01-489-5673
NSN 5930-00-560-4231