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 6685-01-444-1496
NSN 5996-01-295-5971
NSN 6130-01-419-3535
NSN 5905-01-301-5786
NSN 5855-01-614-1661
NSN 4140-00-903-5799
NSN 6135-00-228-8140
NSN 5915-01-358-2467
NSN 6145-01-398-0607
NSN 6145-00-943-9549
NSN 5945-01-483-3247
NSN 6145-01-229-4136