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 6320-00-284-1524
NSN 5915-00-413-2395
NSN 5998-01-123-3036
NSN 6150-01-310-6213
NSN 5998-01-241-2593
NSN 5950-01-069-2784
NSN 6620-01-374-4382
NSN 6685-01-263-8454
NSN 5925-01-566-3242
NSN 5975-00-577-3765
NSN 5950-01-584-6468
NSN 5895-00-508-7838