Flow area is 1.483 min. To 1.492 max. 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 6650-01-645-2850
NSN 5990-01-411-5930
NSN 5930-00-212-8866
NSN 6110-01-181-6216
NSN 5905-01-655-6836
NSN 6620-01-189-8153
NSN 7035-01-073-9424
NSN 5960-01-219-5504
NSN 5910-00-804-5297
NSN 6685-01-392-1513
NSN 5950-01-237-5773
NSN 5915-01-444-4069