Flow area 1.473 - 1.483.Pitch is 34deg 47min 28sec
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 5950-01-501-5682
NSN 5905-01-288-1907
NSN 5935-01-293-5057
NSN 5965-00-142-9052
NSN 6320-01-497-3116
NSN 6320-00-857-4073
NSN 6240-00-933-5823
NSN 5915-01-456-9517
NSN 5835-01-098-9702
NSN 5998-01-628-4898
NSN 5910-01-269-6011
NSN 6130-01-557-5387