Bore diameter 0.533 in.; flange thk 0.045 in.; 8 holes equally spaced 0.175 in.Diameter
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 5835-00-572-7445
NSN 5998-00-284-3804
NSN 5985-01-646-0009
NSN 5990-01-127-4853
NSN 5835-00-438-4489
NSN 5999-01-353-1691
NSN 6645-01-096-9719
NSN 5905-00-503-1779
NSN 6685-01-566-6498
NSN 2925-00-494-5537
NSN 5835-01-435-4139
NSN 5975-01-462-0700