What was found
RIGHT WING LEADING EDGE SKIN AT FUEL ACCESS PANEL FWD INBOARD CORNER HAS A .600 INCH CRACK. INSTALLED REPAIR DOUBLER IAW DWG ARB1232 AND IAW SRM 57-40-02-2R AND SRM 51-31- 01-OG. ORIG SUBMISSION DATE: 1/4/2023
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING LEADING EDGE SKIN AT FUEL ACCESS PANEL FWD INBOARD CORNER HAS A .600 INCH CRACK. INSTALLED REPAIR DOUBLER IAW DWG ARB1232 AND IAW SRM 57-40-02-2R AND SRM 51-31- 01-OG. ORIG SUBMISSION DATE: 1/4/2023