Flow area 1.436-1.446; pitch 34 deg. 11 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 5895-01-099-4102
NSN 5910-01-571-8500
NSN 5998-01-211-8078
NSN 5925-01-320-9138
NSN 6620-01-017-4790
NSN 5975-00-528-9774
NSN 7035-01-202-8172
NSN 5835-01-528-7454
NSN 6220-01-162-7954
NSN 2925-01-289-6448
NSN 6650-01-011-9093
NSN 7035-00-115-1886