1.810 in.Min 1.830 in.Max lg; 0.481 in.Min 0.485 in.Max diameter large end; 0.240 in.Min 0.260 in.Max diameter narrow end;
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 5915-01-462-8937
NSN 6145-01-025-6514
NSN 5935-00-138-4230
NSN 6220-00-935-6881
NSN 5835-00-419-0575
NSN 6110-01-062-7532
NSN 5999-01-570-4979
NSN 6610-00-891-6370
NSN 5990-01-443-2931
NSN 5975-00-185-5243
NSN 6620-01-197-7665
NSN 6620-01-585-3982