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 6610-00-901-5137
NSN 2925-00-035-5633
NSN 5930-00-705-5406
NSN 5910-00-218-1114
NSN 5990-01-541-7671
NSN 5999-01-071-0728
NSN 5925-01-429-0392
NSN 5999-00-175-5053
NSN 5945-01-172-4284
NSN 6105-01-400-0895
NSN 6610-01-259-5296
NSN 5975-01-398-9128