Cres, ams5382, 25 vanes equally spaced, 1.433 in.Nom o/a lg, 7.900 in.Nom o/a od, 3.310 in.Nom id, 6 tangs located on id, 3.310 in.Nom minor diameter tangs, 3.680 in.Nom major diameter tang s
A single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5985-01-421-7570
NSN 5910-01-633-9963
NSN 5950-00-269-4805
NSN 5895-00-868-3668
NSN 5935-01-322-3810
NSN 5835-01-477-0137
NSN 5965-01-460-4172
NSN 5920-00-844-2488
NSN 6320-01-052-2118
NSN 6685-01-643-9898
NSN 5965-01-475-3024
NSN 2925-01-271-8727