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 4140-01-456-0891
NSN 5855-01-325-9507
NSN 6240-01-613-5801
NSN 5945-00-701-7612
NSN 5985-00-581-0513
NSN 5835-00-995-9411
NSN 6135-00-497-0491
NSN 5945-01-503-0423
NSN 5990-00-159-1774
NSN 5996-01-319-3205
NSN 6130-01-298-1826
NSN 6620-01-514-7786