As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFW - FOUND INTERNAL CORROSION ON THE TEE FITTING LOCATED NEXT TO THE AFT FASTENER HOLE. TRIMMED OUT DISCREPANT AREA. APPLIED ALODINE AND PRIMED. FABRICATED AND INSTALLED FILLER, SHIM, AND STRAP USING 7075-T6 ALUMINUM. PRIMED AND PAINTED. ACCOMPLISHED AND APPROVED BY ENGINEERING PER MRB 95C062. TST 41,966.02. CYCLES, 13,544. (X)