What was found
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF L-2 DOOR, STA 986, S7L. THE CRACK WAS ROUTED OUT, DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03510, SRM 51-30-2, AND BOEING DRAWING 65C35747.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF L-2 DOOR, STA 986, S7L. THE CRACK WAS ROUTED OUT, DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03510, SRM 51-30-2, AND BOEING DRAWING 65C35747.