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 6150-01-419-5965
NSN 6135-01-046-6803
NSN 5999-01-432-0891
NSN 5985-00-722-1852
NSN 5910-01-371-6536
NSN 5905-00-697-2761
NSN 6685-01-082-6795
NSN 5975-00-452-9315
NSN 5935-01-497-3402
NSN 5950-01-648-6384
NSN 5915-01-486-4068
NSN 5920-01-316-8286