Bore diameter 0.533 in.; flange thk 0.045 in.; 8 holes equally spaced 0.175 in.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 6150-01-513-9757
NSN 2925-01-538-1343
NSN 6645-01-253-1950
NSN 4140-00-951-3093
NSN 5945-00-065-2127
NSN 5920-00-636-4713
NSN 5950-01-281-7506
NSN 6320-00-845-3261
NSN 5990-01-110-8979
NSN 5998-00-364-7549
NSN 5895-01-245-5315
NSN 7035-00-104-7613