Flow area 1.427-1.436; pitch 34 deg. 2 min. 28 sec.; 2nd end width 0.760-0.780
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 6145-01-010-5474
NSN 5945-01-471-0410
NSN 5920-01-071-5076
NSN 5990-00-697-8883
NSN 6685-01-510-7773
NSN 5920-00-518-3871
NSN 5835-00-401-8655
NSN 5895-00-473-9673
NSN 5835-01-125-6676
NSN 5945-01-247-5814
NSN 5895-00-772-0640
NSN 2925-01-572-5846