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 6135-01-441-0518
NSN 6135-01-100-3593
NSN 6110-00-343-1618
NSN 5920-00-548-9321
NSN 2925-01-344-0281
NSN 6650-00-759-1390
NSN 6220-01-270-3733
NSN 6240-01-055-5193
NSN 5999-01-283-9487
NSN 5930-00-432-0092
NSN 7035-00-585-2113
NSN 5990-01-351-2379