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 5910-01-529-6105
NSN 5990-00-608-4779
NSN 5930-00-833-9808
NSN 4140-01-499-2500
NSN 5998-01-450-8131
NSN 6650-00-500-6455
NSN 5965-01-624-1255
NSN 6320-00-261-9136
NSN 6610-01-538-0016
NSN 5996-00-910-3773
NSN 6130-00-852-6379
NSN 5985-01-230-9419