As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 25 AND RIB 26 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.276. REMOVED MATERIAL 0.003. REMAINING THICKNESS 0.273 AND IS FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PG 68, FIG 7A AND SRM 57-20-12, PARA A-1 (G), FIG 201. ACCOMPLISHED PFPI IAW A310 NTM 51-90-11. ALODINED AND PRIMED IAW SRM 51-20-10 AND SRM 57-20-12; PG 201B; PARA 3(A).