Flow area 1.464 - 1.489.Pitch is 34deg 38min 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 6130-01-272-5233
NSN 6685-00-221-5750
NSN 5905-00-824-1371
NSN 5910-00-450-7379
NSN 5990-00-389-0554
NSN 5999-00-642-1653
NSN 6685-01-445-7658
NSN 5915-01-364-6943
NSN 5905-01-655-4180
NSN 5950-00-075-4591
NSN 5835-00-870-7034
NSN 5915-00-891-3301