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 5905-00-269-3931
NSN 6110-01-465-7511
NSN 5910-01-471-8338
NSN 6150-01-045-1529
NSN 5910-01-527-2988
NSN 5990-01-284-3187
NSN 2925-01-193-6689
NSN 6145-01-501-2931
NSN 6620-00-251-0569
NSN 6320-01-129-9656
NSN 2925-01-535-7235
NSN 6620-01-095-5558