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 5975-00-925-1197
NSN 2925-01-518-3453
NSN 6135-01-479-9783
NSN 6240-00-565-9141
NSN 5999-01-100-6143
NSN 5835-00-993-0040
NSN 5960-01-165-1956
NSN 5910-00-541-1381
NSN 6145-01-446-8680
NSN 5895-01-468-0776
NSN 5895-01-092-2085
NSN 5835-00-170-5238