NAVWEPS 00-EOT-80  OPERATING STRENGTH LIMITATIONS  FATIGUE STRENGTH OF TYPICAL AIRCRAFT METAL  Egu,e 5.1. Strength Chomctorirfics  NUMBER OF APPLICATIONS  TO CAUSE FATIGUE FAILURE  327  ULTIMATE  STRENGTH  -Cc  STRESSES APPLIED ABOVE  THIS POINT RESULT IN  OBJECTIONABLE PERMANENT  DEFORMATION  Q  FAILURE  -I  STRAIN  PERMANENT  (IN/IN)  SET  II:  -I I--  STATIC STRENGTH OF TYPICAL  AIRCRAFT METAL 