Flow area 1.446-1.455; pitch 34 deg. 20 min. 28 sec.; 2nd end width 0.760-0.780 in.
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 6150-01-442-3719
NSN 5930-01-265-6888
NSN 5996-01-370-6593
NSN 6320-01-132-2746
NSN 6150-00-841-6629
NSN 5930-00-276-5567
NSN 5985-01-542-1968
NSN 5960-00-927-6716
NSN 6685-00-928-2241
NSN 5935-01-366-4580
NSN 6320-00-036-3688
NSN 6685-01-038-8482