Flow area is 1.409 min. To 1.418 max. Diameter
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 5935-01-280-5476
NSN 6320-00-295-2854
NSN 5930-00-054-6757
NSN 5985-01-589-6920
NSN 5990-01-542-4212
NSN 5855-01-029-8733
NSN 6620-01-254-3609
NSN 5895-01-213-2387
NSN 5950-01-142-2634
NSN 6110-01-595-1552
NSN 5996-00-978-9705
NSN 6685-00-824-6875