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 6610-00-084-9178
NSN 5915-01-580-0308
NSN 5950-01-461-9565
NSN 5855-00-087-3144
NSN 6110-00-514-2639
NSN 6610-00-186-9180
NSN 5998-01-171-2112
NSN 5975-01-604-2217
NSN 2925-01-317-6973
NSN 6110-01-125-5627
NSN 5895-01-069-9841
NSN 5855-01-391-3819