What was found
LT INBD MIDFLAP COVE LIP PANEL AT OUTBD END CRACKED. STOP DRILLED CRACK/INSTALLED FIBERGLASS OVERLAYS PRIMED AND PAINTED PER SRM 51-40-15 AND 51-24-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT INBD MIDFLAP COVE LIP PANEL AT OUTBD END CRACKED. STOP DRILLED CRACK/INSTALLED FIBERGLASS OVERLAYS PRIMED AND PAINTED PER SRM 51-40-15 AND 51-24-11.