What was found
INSPECTION FOUND A 1 INCH CRACK IN LT WHEEL WELL FORWARD JAMB SUPPORT. AN ANGLE AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-11, 51-10-03, AND 53-10-01, FIGURE 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 WHEEL WELL FORWARD JAMB SUPPORT. AN ANGLE AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-11, 51-10-03, AND 53-10-01, FIGURE 2.