What was found
AFT WING TO FUSELAGE PANEL 195DL ANGLE PN CC690-39251-1IS CRACKED. REMOVED AND REPLACED THE ANGLE, AND AFT JOINT STRAP IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, DRAWING CC690-39171 AND REO 690-53-82-052.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT WING TO FUSELAGE PANEL 195DL ANGLE PN CC690-39251-1IS CRACKED. REMOVED AND REPLACED THE ANGLE, AND AFT JOINT STRAP IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, DRAWING CC690-39171 AND REO 690-53-82-052.