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 6650-01-305-0027
NSN 5855-01-506-4610
NSN 5920-01-569-2896
NSN 5999-00-834-9854
NSN 6240-01-506-9294
NSN 5855-01-492-9795
NSN 6150-01-016-4445
NSN 6685-01-352-7241
NSN 6650-01-525-7370
NSN 6110-01-416-0683
NSN 5855-01-249-0717
NSN 5975-01-377-2524