What was found
INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SKIN ABOVE NR 1 ENGINE PYLON AT STA 1401. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3, 53-10-3, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SKIN ABOVE NR 1 ENGINE PYLON AT STA 1401. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3, 53-10-3, AND 51-30-2.