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 5925-01-160-6243
NSN 6610-00-194-0068
NSN 5965-00-234-7338
NSN 5925-00-666-4753
NSN 6130-00-528-7838
NSN 4140-01-188-0111
NSN 6650-01-584-3208
NSN 5920-01-173-1014
NSN 6620-01-253-0374
NSN 5999-00-518-5419
NSN 5996-00-608-6425
NSN 6220-01-233-7456