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 5950-00-170-6790
NSN 6685-01-076-8967
NSN 5855-01-027-1571
NSN 5965-01-032-7236
NSN 6145-00-008-1834
NSN 5975-00-099-9312
NSN 6145-00-398-4405
NSN 5998-01-387-8466
NSN 5990-01-334-4111
NSN 5855-00-127-5559
NSN 5935-00-647-4020
NSN 5996-00-388-6552