Flow area 1.418-1.427; pitch 33 deg. 53 min. 28 sec.
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 5945-01-481-2280
NSN 5950-01-352-8520
NSN 5999-00-553-3946
NSN 5990-01-146-9126
NSN 5985-01-259-2057
NSN 6105-00-753-8756
NSN 5935-01-504-1168
NSN 6610-01-566-8198
NSN 5910-01-424-7249
NSN 5999-01-381-3866
NSN 7035-01-426-4133
NSN 6110-01-172-1383