T.O. 2j-f100-24, fig 92, ind 16a; used on the augmentor combustion chamber duct; use only on p/n 4067029
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 5945-01-508-9384
NSN 5990-01-387-3820
NSN 6685-01-065-3511
NSN 5935-01-446-5148
NSN 5855-01-337-0245
NSN 6220-01-359-1593
NSN 6610-01-320-6628
NSN 5895-00-520-4341
NSN 5895-00-852-4237
NSN 5960-01-502-6270
NSN 6645-00-419-4860
NSN 6645-01-073-0597