What was found
INSPECTION FOUND A HOLE CHAFED IN SKIN FORWARD OF FLUX VALVE, RT WING TIP. THE DAMAGED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A HOLE CHAFED IN SKIN FORWARD OF FLUX VALVE, RT WING TIP. THE DAMAGED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-5.