5.798 o/a dia; t.O. 2j-tf39-4; goes on the combustion chamber and in the hhigh pressure turbine
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 5895-01-122-5582
NSN 6320-00-218-6105
NSN 6145-00-674-1807
NSN 6145-01-379-6123
NSN 6685-01-351-1143
NSN 6220-00-928-9356
NSN 5985-01-589-6029
NSN 5905-01-399-0239
NSN 5999-00-782-7919
NSN 6145-01-278-6903
NSN 6610-00-221-6124
NSN 5925-01-323-1613