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 5915-01-367-2056
NSN 5855-01-217-6857
NSN 5920-01-377-8491
NSN 5935-01-313-8404
NSN 6135-01-512-8740
NSN 5950-01-541-5016
NSN 2925-00-275-1807
NSN 5930-01-384-4339
NSN 5990-01-455-8035
NSN 5965-01-240-0233
NSN 6610-01-194-3759
NSN 5920-00-081-5958