Flow area 1.427-1.436; pitch 34 deg. 2 min. 28 sec.; 2nd end width 0.760-0.780
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 4140-01-447-8033
NSN 6135-00-752-1589
NSN 5925-00-764-3001
NSN 5935-01-250-6643
NSN 5920-01-546-2251
NSN 4140-00-420-0251
NSN 5925-01-345-1422
NSN 5895-01-074-5110
NSN 5925-00-318-3023
NSN 5905-01-266-7778
NSN 5895-00-441-9714
NSN 5910-00-824-7740