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 5895-01-058-5584
NSN 5996-01-592-3011
NSN 5895-00-959-2284
NSN 5915-00-251-8191
NSN 5920-00-156-4482
NSN 5895-01-592-3034
NSN 5960-01-094-7569
NSN 6650-00-397-0372
NSN 5855-00-586-6255
NSN 6145-01-389-8026
NSN 4140-01-087-0359
NSN 5945-00-148-8285