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NUTS, SELF-LOCKING, ALLOY, CORROSION AND HEAT RESISTANT High Strength, Prevailing Torque, All Metal 1400° F (760° C) Use, Unified "J" (MIL-S-8879) Thread Form

  • Aerospace Material Specification
  • AMS7253A
  • Revised
Published May 15, 1973 by SAE International in United States
 
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Language: English