What was found
LEFT WING OUTBOARD PANEL DELAMINATED. REMOVED DAMAGED AREA OF SKIN PER SRM 51 40 24. MADE REPAIR PARTS TREATED WITH AC 130 SOLGEL. REF SRM 51 40 20, PG 42 46. APPLIED PRIMER BARED AFT 175* PER SRM 51 40 24 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING OUTBOARD PANEL DELAMINATED. REMOVED DAMAGED AREA OF SKIN PER SRM 51 40 24. MADE REPAIR PARTS TREATED WITH AC 130 SOLGEL. REF SRM 51 40 20, PG 42 46. APPLIED PRIMER BARED AFT 175* PER SRM 51 40 24 FIG 2.