What was found
LEFT OVERWING PANEL UPPER FUSELAGE SUPPORT CRACKED BETWEEN FRAME 41 & 42. REPAIRED IAW SRM 53-23-12. SEE TURNOVER FOR DETAILS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT OVERWING PANEL UPPER FUSELAGE SUPPORT CRACKED BETWEEN FRAME 41 & 42. REPAIRED IAW SRM 53-23-12. SEE TURNOVER FOR DETAILS.