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 5915-00-679-9390
NSN 7035-01-407-6413
NSN 6650-01-113-7563
NSN 5999-00-286-6231
NSN 7035-01-085-5955
NSN 5930-01-285-8193
NSN 6240-01-226-2902
NSN 5945-01-067-7955
NSN 5990-01-414-7618
NSN 5915-01-460-4392
NSN 5975-01-165-0414
NSN 5998-00-451-7006