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 4140-01-425-1607
NSN 6320-01-296-3181
NSN 5985-00-853-3558
NSN 6150-01-580-7989
NSN 7035-01-649-8977
NSN 5996-01-247-7671
NSN 5998-01-379-4301
NSN 5975-01-233-1811
NSN 5855-01-413-3352
NSN 6645-01-438-6986
NSN 6650-01-044-9860
NSN 5985-00-085-1710