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 6320-01-585-8468
NSN 6240-00-179-5043
NSN 5895-01-389-1166
NSN 5910-00-155-2562
NSN 6610-01-246-9933
NSN 5905-00-844-4815
NSN 7035-01-435-4009
NSN 5945-01-228-5470
NSN 6645-00-927-8207
NSN 6220-01-376-9287
NSN 6240-01-296-3975
NSN 6240-01-448-9636