What was found
C-CHECK, LT WING VERIFY POSSIBLE CRACK ON FITTING FROM O/B FLAP STA 406.000. PERFORMED HFEC INSPECTION IAW DC-8 NON-DESTRUCTIVE TESTING STANDARD PRACTICE MANUAL PART 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK, LT WING VERIFY POSSIBLE CRACK ON FITTING FROM O/B FLAP STA 406.000. PERFORMED HFEC INSPECTION IAW DC-8 NON-DESTRUCTIVE TESTING STANDARD PRACTICE MANUAL PART 6.