What was found
LEFT WING LATERAL PANEL UPPER ATTACH ANGLE CRACKED BEWTEEN FUSELAGE FRAMES 48 AND 49. COMPLETED A REPAIR TO THE ATTACH ANGLE BETWEEN FUSELAGE FRAMES 48-49 IAW SRM 53-23-12 TYPE II.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LATERAL PANEL UPPER ATTACH ANGLE CRACKED BEWTEEN FUSELAGE FRAMES 48 AND 49. COMPLETED A REPAIR TO THE ATTACH ANGLE BETWEEN FUSELAGE FRAMES 48-49 IAW SRM 53-23-12 TYPE II.