1.500 thickness x 1.500 width x 16.000 length bar stock, 4340 steel condition c
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 5905-00-715-1119
NSN 6610-01-278-9704
NSN 6135-01-613-1464
NSN 5996-01-068-2886
NSN 6220-01-280-8458
NSN 5910-00-211-1274
NSN 6685-01-386-5129
NSN 5990-01-378-7349
NSN 5920-01-174-8540
NSN 5935-00-505-0815
NSN 6240-01-360-6965
NSN 5935-01-045-2702