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 5915-00-233-4501
NSN 5915-00-124-5266
NSN 5915-01-374-5983
NSN 6620-00-170-5296
NSN 6685-00-598-1944
NSN 6150-01-426-8986
NSN 5950-01-299-4799
NSN 5920-01-575-3510
NSN 6220-00-428-5943
NSN 6620-01-271-8984
NSN 6620-00-209-0767
NSN 4140-01-515-8673