Turbine fram assembly
An item specifically designed to position and/or restrain the movement of one or more vane,vane segment, or vane assembly, fan, aircraft gas turbine engine. It may be the full 360 degrees required for one fan stage or a segment thereof.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5950-00-950-6040
NSN 6320-00-098-2858
NSN 5950-00-865-2681
NSN 5835-00-764-4388
NSN 5855-01-115-9014
NSN 5999-00-702-8988
NSN 5855-01-653-7718
NSN 6150-00-205-6775
NSN 5945-01-299-2798
NSN 2925-01-125-2973
NSN 5930-01-130-7838
NSN 5855-01-100-3272