What was found
INSPECTION FOUND A 0.3 INCH CRACK IN C-2 DOOR AT LIGHTENING HOLE LOCATED AT ACCESS TO SPRING SUPPORT FITTING. THE CRACKED AREA WAS TRIMMED AND DRESSED UP AND A DOUBLER WEB REPAIR WAS INSTALLED IAW SRM 51-70-13.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.3 INCH CRACK IN C-2 DOOR AT LIGHTENING HOLE LOCATED AT ACCESS TO SPRING SUPPORT FITTING. THE CRACKED AREA WAS TRIMMED AND DRESSED UP AND A DOUBLER WEB REPAIR WAS INSTALLED IAW SRM 51-70-13.