Flow area 1.418-1.427; pitch 33 deg. 53 min. 28 sec.
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 5915-01-349-5676
NSN 6610-00-199-8915
NSN 5990-01-478-8638
NSN 6105-00-357-1801
NSN 6685-01-424-1542
NSN 5965-01-560-6491
NSN 5990-00-583-9577
NSN 6620-01-550-2804
NSN 7035-01-283-2536
NSN 5930-00-686-2940
NSN 5950-01-342-8380
NSN 5990-00-366-0112