What was found
LT WING UPPER L/E PANEL HAS A PREVIOUS REPAIR DELAMINATED AND CRACKED, 8.0 IN. BY 5.0 IN. ACCOMPLISHED PERMANENT REPAIR AS PER B747 SRM 51-40-09 FIG 1 AND B747 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO 4757A335.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING UPPER L/E PANEL HAS A PREVIOUS REPAIR DELAMINATED AND CRACKED, 8.0 IN. BY 5.0 IN. ACCOMPLISHED PERMANENT REPAIR AS PER B747 SRM 51-40-09 FIG 1 AND B747 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO 4757A335.