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 5945-00-502-4484
NSN 5950-01-442-6188
NSN 6240-01-117-7150
NSN 6105-01-574-5670
NSN 5920-01-050-7474
NSN 5905-00-347-7311
NSN 6150-00-405-6399
NSN 6650-01-033-2979
NSN 6645-00-755-9782
NSN 6620-00-527-9280
NSN 6135-00-567-1322
NSN 5905-01-152-0578