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 6220-01-004-6234
NSN 5855-01-425-1330
NSN 5930-01-657-0685
NSN 6610-01-483-1317
NSN 6135-01-142-6456
NSN 6645-01-215-9938
NSN 6110-00-239-5548
NSN 6145-00-134-7271
NSN 5920-00-518-0839
NSN 6150-01-486-5380
NSN 6110-01-247-6109
NSN 6150-01-134-5239