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 4140-01-291-4838
NSN 6130-01-370-4756
NSN 5920-01-460-5495
NSN 5925-01-569-2981
NSN 5915-01-564-8637
NSN 6220-01-214-0270
NSN 6135-00-255-1340
NSN 5985-00-232-4867
NSN 6110-00-394-7187
NSN 5915-01-170-6753
NSN 6220-01-554-2501
NSN 6105-01-071-5565