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 5925-00-924-9596
NSN 5910-00-296-1054
NSN 6145-01-499-9745
NSN 5895-00-254-5001
NSN 5935-01-142-7419
NSN 6645-01-591-3970
NSN 5855-01-341-7320
NSN 5999-01-287-4327
NSN 6130-01-422-2603
NSN 5975-00-189-0857
NSN 5975-00-442-3500
NSN 5925-01-285-0362