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 6105-01-006-7069
NSN 7035-00-465-3298
NSN 5945-01-468-5372
NSN 5930-00-880-9878
NSN 5985-01-166-1905
NSN 6105-01-546-0591
NSN 5965-01-038-1904
NSN 2925-01-273-4898
NSN 5935-01-300-4153
NSN 5930-00-283-0962
NSN 6240-01-646-5509
NSN 5915-01-137-3709