What was found
LT WING PANEL CORROSION. REMOVED DAMAGED SKIN. ACCOMPLISHED STEPS 1-6 OF EO DC8-5720-29785 APPENDIX A. ACCOMPLISHED REPAIR STEPS 1-9 OF EO DC8-5720-29785-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING PANEL CORROSION. REMOVED DAMAGED SKIN. ACCOMPLISHED STEPS 1-6 OF EO DC8-5720-29785 APPENDIX A. ACCOMPLISHED REPAIR STEPS 1-9 OF EO DC8-5720-29785-A.