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 5915-01-472-4169
NSN 6685-01-598-5130
NSN 5990-00-153-0055
NSN 6105-01-461-8426
NSN 5920-01-209-2990
NSN 6320-01-648-5538
NSN 4140-01-070-4928
NSN 5996-01-647-9465
NSN 6110-01-453-9302
NSN 6320-01-141-3791
NSN 6620-00-245-6164
NSN 5985-00-707-3473