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TF-33 aircraft engine
matl steel, AMS6322; hardenss rc 35.0-40.0; nickel cadmium plate, AMS2416; modified per PWA-S-2416, fs; length 11.835-11.837; 0.496-0.497 in. dia. 5 lands; 0.410-0.420 in. dia. 4 grooves; threaded 0.500-20 UNF-03A both ends; used on the compressor ROTOR-Front
1EA
FSC 5307 ⁓ Studs
Used on tf-33 aircraft engine. matl steel, AMS6322; hardenss rc 35.0-40.0; nickel cadmium plate, AMS2416; modified per pwa-s-2416, fs; length 11.835-11.837; 0.496-0.497 in. dia. 5 lands; 0.410-0.420 in. dia. 4 grooves; threaded 0.500-20 unf-03a both ends; used on the compressor rotor-front
1. | 463553 | Cage 77445 |
Nothing similar to this part number was found in our inventory
A headless fastener not exceeding 12 inches (304.8 mm) in length, threaded externally on both ends with threads of the same nominal diameter. all or part of the unthreaded section has a cross-sectional diameter greater than the nominal stud size plus 0.020 inches (0.508 mm). it may be thread relieved. see also stud, locked in.