Flow area is 1.409 min. To 1.418 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 5985-01-126-3124
NSN 7035-01-428-2336
NSN 5985-01-649-7320
NSN 6135-01-415-1163
NSN 6320-01-132-2746
NSN 6110-01-207-1404
NSN 6130-00-212-4883
NSN 5985-00-032-7023
NSN 7035-01-145-5059
NSN 6240-00-292-3237
NSN 2925-00-152-1825
NSN 5925-01-641-5779