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 5999-01-112-1015
NSN 6320-00-242-3300
NSN 6685-01-010-0451
NSN 6620-00-957-4239
NSN 5895-01-330-1864
NSN 5920-01-227-1877
NSN 6645-01-298-3811
NSN 6135-00-315-1187
NSN 5996-00-008-7960
NSN 6145-01-492-9840
NSN 5910-01-101-3092
NSN 6650-01-421-4024