What was found
LEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW ES00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW ES00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.