What was found
EVIDENCE OF WEAR ON CENTER FLANGE OF ADAPTER AT FRAME 27 BETWEEN Y1456 AND Y1959. DAMAGE REMOVED IAW SRM 51-23-10. ADAPTER PLATE REPLACED IAW SRM 51-40-21 AND DWG A53781920 .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EVIDENCE OF WEAR ON CENTER FLANGE OF ADAPTER AT FRAME 27 BETWEEN Y1456 AND Y1959. DAMAGE REMOVED IAW SRM 51-23-10. ADAPTER PLATE REPLACED IAW SRM 51-40-21 AND DWG A53781920 .