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 6610-01-594-6999
NSN 5999-00-205-0918
NSN 5835-00-247-0161
NSN 6145-01-224-1829
NSN 6620-01-200-6493
NSN 6220-01-655-8981
NSN 5996-00-225-3286
NSN 6240-01-331-2244
NSN 7035-01-263-5463
NSN 5975-01-381-2763
NSN 2925-01-544-4880
NSN 6220-00-199-9401