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 5945-01-275-3080
NSN 5999-00-907-9452
NSN 5905-01-089-8723
NSN 6130-01-372-4266
NSN 6135-00-803-3012
NSN 6150-01-264-5550
NSN 5915-01-573-9227
NSN 5855-00-631-4565
NSN 7035-01-569-3875
NSN 7035-01-482-1356
NSN 5975-01-592-2288
NSN 6240-01-605-4455