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 5915-00-308-2469
NSN 5935-01-483-4027
NSN 5920-00-061-8623
NSN 5998-00-227-4944
NSN 5960-01-053-4358
NSN 6610-01-242-9674
NSN 5930-01-093-6699
NSN 6145-01-148-7837
NSN 5905-01-646-4016
NSN 5990-01-234-8646
NSN 5975-01-333-4077
NSN 5999-01-013-2581