1.446-1.455 sq. In. Flow area
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 6620-01-444-7053
NSN 5990-01-652-7373
NSN 6240-00-551-3144
NSN 5925-00-222-8263
NSN 5855-01-286-9928
NSN 5855-01-648-2674
NSN 6150-00-636-8938
NSN 5895-00-654-5812
NSN 5935-01-177-3494
NSN 5975-01-299-7429
NSN 5999-01-017-2377
NSN 6240-00-102-4003