Nickle alloy, m3602 fscm 91547, rockwell c scale 35 min, 40 maxhardness
A component of a vane assembly, fan, aircraft gas turbine engine. It is designed to receive air from the preceding fan blades and deliver it to the succeeding row of fan blades or compressor at correct pressure, velocity and direction.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5835-01-632-6627
NSN 5835-01-642-4705
NSN 5998-01-222-1993
NSN 5990-01-434-3469
NSN 5910-01-241-0565
NSN 5910-01-275-7259
NSN 5930-00-250-9605
NSN 6685-01-634-0611
NSN 6240-01-123-8822
NSN 6135-00-477-8847
NSN 5930-01-441-9814
NSN 5910-01-513-4684