As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON SKIN OF RT MAIN GEAR STRUT DOOR BELOW RUBSTRIP. DOOR WAS REMOVED IAW AMM 32-12-01. CORROSION OF RT MAIN GEAR STRUT DOOR WAS REMOVED IAW SRM 52-01. AREA WAS MEASURED IAW NDT SPM 04-00-07. ORIGINAL THICKNES 0.063 REMAINING THICKNESS 0.041. THEREFORE ITS OUT OF LIMITS IAW SRM 52-01 AND RT MAIN GEAR STRUT WAS REPLACED IAW AMM 32-12-01 AND WILL BE CHECKED AND ADJUSTED.