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 6645-00-248-5434
NSN 6620-00-086-5223
NSN 6685-01-569-7986
NSN 2925-00-791-8776
NSN 2925-01-429-2235
NSN 5985-01-130-9218
NSN 6145-00-291-5388
NSN 6130-01-055-5272
NSN 5990-01-139-6042
NSN 6320-01-532-6746
NSN 6130-01-524-3058
NSN 5975-01-354-6251