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 5945-01-595-2194
NSN 5930-01-022-5293
NSN 6620-01-426-2220
NSN 5965-00-422-5415
NSN 5975-01-483-1515
NSN 6105-01-423-8242
NSN 6620-01-480-6887
NSN 6650-01-003-9355
NSN 5996-01-391-7489
NSN 6320-01-349-8077
NSN 5835-01-222-2437
NSN 5855-01-236-3364