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 6130-01-359-6562
NSN 6650-00-665-3658
NSN 5950-01-074-8464
NSN 5996-00-437-3668
NSN 6685-01-484-2326
NSN 6645-01-463-3441
NSN 5998-01-312-4142
NSN 6320-01-631-7828
NSN 6240-00-186-3245
NSN 6105-01-307-8086
NSN 5965-01-197-6924
NSN 5920-01-459-2299