Inconel 625 ams5599; 29.900 in.Lg, 26.280 in.Dia o/a; 30 holes 0.221 in.Dia on a 25.860 in.Dia bolt circle;
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 5925-00-283-1400
NSN 5998-01-062-0607
NSN 5835-01-261-9878
NSN 5920-01-338-7459
NSN 5999-00-904-4210
NSN 5930-01-564-5786
NSN 5920-01-323-5351
NSN 6620-01-446-6571
NSN 6685-01-122-8331
NSN 6110-00-045-6323
NSN 6320-01-322-8340
NSN 6240-01-177-6386