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 5990-00-965-0495
NSN 5965-01-354-9834
NSN 6685-01-094-2784
NSN 6240-00-456-6238
NSN 5990-01-474-3477
NSN 5835-01-442-6482
NSN 6320-00-857-4073
NSN 5990-01-443-2931
NSN 5915-00-333-8618
NSN 5910-00-757-2741
NSN 7035-00-529-3128
NSN 5965-01-109-2917