What was found
LT MIDFLAP COVE LIP PANEL INBD HAS CRACK. CLEANED/SMOOTHED DAMAGED AREA. STOP DRILLED CRACK, APPLIED FIBERGLASS OVERLAY 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 MIDFLAP COVE LIP PANEL INBD HAS CRACK. CLEANED/SMOOTHED DAMAGED AREA. STOP DRILLED CRACK, APPLIED FIBERGLASS OVERLAY AND PAINTED PER SRM 51-40-15 AND 51-24-11.