As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 83" FROM I/B END AND 8" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-01-2R AND 51-70- 07-0G. MAJOR REPAIR