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 6320-00-036-3688
NSN 5996-01-149-2434
NSN 5990-00-038-6482
NSN 2925-01-113-6904
NSN 5905-00-268-2535
NSN 6685-00-001-8037
NSN 5925-01-539-9181
NSN 5910-01-364-1947
NSN 5985-01-546-3192
NSN 6220-01-063-7287
NSN 5950-00-816-9288
NSN 5895-01-409-2949