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 5960-01-273-7044
NSN 6645-00-411-3733
NSN 5990-00-583-3412
NSN 6620-01-328-3621
NSN 5925-00-407-2192
NSN 6105-00-186-0161
NSN 2925-01-442-4171
NSN 5895-01-042-8622
NSN 6645-00-935-7046
NSN 6105-00-933-5161
NSN 5835-00-289-9080
NSN 5999-00-435-2540