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 5915-01-186-4199
NSN 5998-01-123-4244
NSN 6240-01-448-5273
NSN 6320-00-110-8005
NSN 6610-00-833-5498
NSN 6150-00-506-0941
NSN 5905-00-253-4247
NSN 6130-01-641-5764
NSN 6685-01-153-1846
NSN 6320-00-831-2227
NSN 5895-00-137-6368
NSN 6620-01-201-6080