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 6610-01-120-7670
NSN 2925-01-448-2880
NSN 6240-00-141-6143
NSN 6130-00-972-3069
NSN 5960-01-100-7381
NSN 6685-00-186-9190
NSN 5835-01-555-8963
NSN 6610-01-558-1815
NSN 5910-01-218-2978
NSN 6645-00-350-8070
NSN 6145-00-715-1186
NSN 6320-01-585-8468