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 5999-00-121-2152
NSN 5975-01-158-6150
NSN 6650-01-015-1589
NSN 5920-01-634-0250
NSN 5950-01-525-2253
NSN 7035-01-547-5361
NSN 4140-01-264-4952
NSN 5835-01-015-0845
NSN 5990-00-287-9259
NSN 5930-01-354-9342
NSN 7035-01-287-9817
NSN 6610-00-681-0590