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 6650-01-212-3964
NSN 5895-01-579-3889
NSN 6110-01-451-4326
NSN 6145-00-551-5288
NSN 6220-00-155-4524
NSN 5950-01-532-7666
NSN 5895-01-120-5290
NSN 5999-00-753-7450
NSN 5985-01-605-2470
NSN 6130-00-402-8545
NSN 5990-01-633-9503
NSN 5945-00-845-1670