What was found
LEFT WING INBOARD MIDFLAP INBOARD UPPER STRESS PANEL PUNCTURED. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING INBOARD MIDFLAP INBOARD UPPER STRESS PANEL PUNCTURED. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-06.