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 6645-00-942-1039
NSN 4140-01-096-1596
NSN 5990-01-432-4984
NSN 5985-01-521-3694
NSN 6685-01-090-1203
NSN 5985-01-371-3449
NSN 5990-01-633-9503
NSN 6645-01-631-3451
NSN 5990-01-320-1412
NSN 5925-01-137-2234
NSN 6645-01-266-8831
NSN 5965-00-929-9415