Flow area 1.418-1.427; pitch 33 deg. 53 min. 28 sec.
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 6105-01-103-3127
NSN 6240-01-074-6550
NSN 6220-01-465-9283
NSN 5985-00-644-9752
NSN 6645-00-216-6126
NSN 6135-01-583-9620
NSN 5990-01-294-6198
NSN 5990-01-067-6015
NSN 6685-00-631-0532
NSN 5950-01-502-6915
NSN 4140-00-694-1936
NSN 5910-00-597-4944