1.446-1.455 sq. In. Flow area
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 5920-01-656-8448
NSN 5925-01-219-0843
NSN 5905-01-222-3387
NSN 5935-01-641-4182
NSN 5910-00-932-2288
NSN 6105-01-442-1250
NSN 5905-01-006-2728
NSN 5855-01-467-3802
NSN 6320-01-056-1164
NSN 6620-01-610-5081
NSN 6645-00-536-1555
NSN 5945-01-481-9061