Flow area 1.446-1.455; pitch 34 deg. 20 min. 28 sec.; 2nd end width 0.760-0.780 in.
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 5945-01-211-5823
NSN 5925-01-510-4579
NSN 5975-00-248-5590
NSN 6130-01-089-8154
NSN 5960-01-361-6543
NSN 5998-01-592-8396
NSN 5999-00-176-2335
NSN 5960-00-125-9335
NSN 5990-00-059-3449
NSN 6645-01-437-9017
NSN 5910-01-551-1473
NSN 6110-01-534-4528