What was found
LEFT WING ATTACHING ANGLE FOR L/E PANEL 523 HB IS CRACKED. FABRICATED A NEW REINFORCING PLATE IAW AIRBUS DWG 23-A-572-43292 ISSUE F. PRIMED IAW A310 SRM 51-21-10 AND 51-23-10. REPLACED REINFORCING PLATE IAW A310 SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING ATTACHING ANGLE FOR L/E PANEL 523 HB IS CRACKED. FABRICATED A NEW REINFORCING PLATE IAW AIRBUS DWG 23-A-572-43292 ISSUE F. PRIMED IAW A310 SRM 51-21-10 AND 51-23-10. REPLACED REINFORCING PLATE IAW A310 SRM 51-40-21.