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 5965-00-111-2073
NSN 5965-00-396-3411
NSN 5855-01-360-6650
NSN 5990-01-197-5901
NSN 6110-01-299-1655
NSN 6685-00-881-3767
NSN 5945-00-164-9775
NSN 6320-00-371-8335
NSN 5965-00-901-6203
NSN 5935-00-005-7283
NSN 5935-00-528-1181
NSN 5855-01-027-1571