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 6650-00-382-1633
NSN 5910-00-598-3674
NSN 2925-01-391-9247
NSN 6645-01-112-3242
NSN 6220-00-386-0997
NSN 6645-01-281-0389
NSN 5960-00-439-5705
NSN 5965-00-698-0433
NSN 5905-01-461-4082
NSN 5950-01-400-5942
NSN 5855-00-151-3853
NSN 6150-01-214-0363