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 6110-01-209-9136
NSN 6320-01-536-3077
NSN 6645-00-591-8036
NSN 5950-01-367-1870
NSN 5895-01-415-2221
NSN 2925-01-327-3069
NSN 5920-01-005-0161
NSN 6320-01-606-2508
NSN 5996-00-567-4804
NSN 5990-01-458-2531
NSN 5915-01-499-2205
NSN 6145-01-219-7743