What was found
AT C-CHECK, LEFT WING FRONT SPAR WS 115 LOWER END OF VERTICAL ANGLE CRACKED. STOP DRILLED END OF CRACK, HFEC, FABRICATED ANGLE REPAIR, 6 X 2 PER SRM 51-40-3. N/R 1648.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LEFT WING FRONT SPAR WS 115 LOWER END OF VERTICAL ANGLE CRACKED. STOP DRILLED END OF CRACK, HFEC, FABRICATED ANGLE REPAIR, 6 X 2 PER SRM 51-40-3. N/R 1648.