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 5935-01-629-0208
NSN 5965-00-630-7872
NSN 5905-00-827-4851
NSN 5996-01-463-0522
NSN 4140-01-277-6355
NSN 6320-01-361-7467
NSN 5910-01-044-0575
NSN 5950-01-006-7865
NSN 5960-01-375-6815
NSN 5996-00-951-9181
NSN 7035-01-657-4665
NSN 5905-01-437-7102