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 5910-01-355-0345
NSN 5965-00-791-0964
NSN 5998-01-303-2551
NSN 5975-01-268-0687
NSN 5975-01-123-8587
NSN 5935-01-585-2031
NSN 5999-00-259-3557
NSN 6240-00-677-0305
NSN 5895-00-837-2343
NSN 5835-01-047-8343
NSN 6685-00-993-5548
NSN 5965-01-305-7413