What was found
INSPECTION FOUND A .5 AND 1 INCH CRACK IN RT FUSELAGE SKIN JUST BELOW PANEL NR 9516, RT SIDE NR 2 ENGINE INLET. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 AND 1 INCH CRACK IN RT FUSELAGE SKIN JUST BELOW PANEL NR 9516, RT SIDE NR 2 ENGINE INLET. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-3.