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 4140-01-213-6162
NSN 5930-01-236-4659
NSN 5925-00-004-7703
NSN 5855-01-373-4610
NSN 5945-01-391-7993
NSN 5999-01-591-9557
NSN 6320-00-213-0477
NSN 6135-00-299-6918
NSN 5999-01-028-0803
NSN 6610-00-968-6149
NSN 5930-01-309-5553
NSN 6130-01-575-3890