Matl steel, ams 6322 or ams 6323; diameter 6.550-6.570; length or width 0.779-0.811; chromium plate optional, ams2406; used on the compressor rotor-front; t.O. 2j-57-4
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 6110-01-069-2966
NSN 5920-00-541-1119
NSN 5925-00-147-7452
NSN 6650-01-525-0958
NSN 6650-01-092-4525
NSN 5975-01-568-1983
NSN 6320-01-366-5157
NSN 6610-01-487-8879
NSN 6320-01-447-4289
NSN 5905-00-543-1096
NSN 6610-01-013-8922
NSN 5975-01-116-1746