What was found
INSPECTION FOUND A .25 INCH CRACK AT RIVET HOLE OF LT ELEVATOR LOWER SKIN JUST AFT OF PANEL NR 9310. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-20-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK AT RIVET HOLE OF LT ELEVATOR LOWER SKIN JUST AFT OF PANEL NR 9310. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-20-3.