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 6685-01-194-3931
NSN 6130-01-618-3004
NSN 4140-01-310-3330
NSN 5965-01-038-5994
NSN 5930-00-215-2881
NSN 6135-01-098-3020
NSN 5965-01-458-2412
NSN 5945-00-362-7192
NSN 5999-01-492-5696
NSN 6320-00-025-9910
NSN 5930-00-048-7904
NSN 5920-00-127-3846