As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT OTBD T/E FOREFLAP HAD GOUGE IN L/E AT WS 550. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 57-50-4, FIG 1. REMOVED DAMAGED AREA. FABRICATED DOUBLER FROM .050 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TREATMENT IAW BSRM 51-10-2. INSTALLED DOUBLER. REBALANCE OF FLAP NOT REQUIRED. NO WEIGHT AND BALANCE CHANGE. (X)