Flow area is 1.483 min. To 1.492 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 5999-01-631-2537
NSN 5985-01-403-2835
NSN 5990-00-795-3796
NSN 5998-01-144-7362
NSN 5998-00-974-2232
NSN 2925-00-947-0263
NSN 5985-01-353-9644
NSN 6150-01-644-0624
NSN
NSN 6650-00-557-5482
NSN 5895-01-634-0630
NSN 6130-00-284-1629