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 5855-01-600-0003
NSN 6150-01-170-5658
NSN 5915-01-525-0479
NSN 5945-00-964-8677
NSN 6220-01-288-8859
NSN 6150-00-325-8597
NSN 6130-00-107-3512
NSN 5925-01-023-1411
NSN 5996-00-007-9845
NSN 5925-01-340-0894
NSN 5996-01-598-9071
NSN 5950-00-397-9869