1.50" thickness x 2.50" width x 11.00" length bar stock, 4340 steel condition c sae ams-s-6415
A rigid piece designed to resist pressure in the direction of its length. it is positioned between the inner and outer rings and is a main component of a frame, front, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 7035-01-065-3744
NSN 6130-01-476-8857
NSN 6135-01-436-7733
NSN 4140-01-388-0835
NSN 5950-00-179-1331
NSN 5985-01-317-3143
NSN 5895-01-258-8869
NSN 5920-01-459-2299
NSN 5935-00-170-7173
NSN 6135-01-111-1495
NSN 5935-01-336-6226
NSN 6685-01-401-5360