What was found
CRACK IN FIBERGLASS CLOSE OUT PANEL FOR FUSELAGE SKIN AT UPPER FORWARD CORNER - L1 DOOR FRAME. REPAIRED WITH FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FIBERGLASS CLOSE OUT PANEL FOR FUSELAGE SKIN AT UPPER FORWARD CORNER - L1 DOOR FRAME. REPAIRED WITH FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.