What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN ABOVE L-2 DOOR UPPER HINGE, STA 947.5, S11L T0 14L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-60-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN ABOVE L-2 DOOR UPPER HINGE, STA 947.5, S11L T0 14L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-60-01.