What was found
INSPECTION FOUND A .25 INCH CRACK NEAR WING SKIN PANEL 515AB HOLE. A REPAIR WAS PERFORMED IAW SRM 57-00-01, FIGURE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK NEAR WING SKIN PANEL 515AB HOLE. A REPAIR WAS PERFORMED IAW SRM 57-00-01, FIGURE 4.