T.O. 2j-f100-14, fig 130 ind 23; 7.2935-7.3319 sq in.; no. 5 bearing
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 5985-00-081-9142
NSN 5925-00-118-8059
NSN 5960-01-201-5804
NSN 5990-00-119-5699
NSN 5950-01-522-1267
NSN 6220-01-120-2325
NSN 6135-01-377-3862
NSN 5935-00-121-7792
NSN 6145-01-484-8735
NSN 6610-00-784-8296
NSN 5950-00-585-9598
NSN 5996-00-802-6095