What was found
RIGHT WING TRAILING EDGE FUSELAGE RUB PLATE FOR TRAILINGEDGEFLAPS HAS MULTIPLE SPOTS OF EXFOLIATION CORROSION VISIBLE. RH RUBPLATE CORROSION REMOVED AND BLENDED IAW SRM 53-40-05-1A-2-5. FASTENER HOLES STOP DRILLED COMPLETE AND DIMPLE WASHERS ADDAED AT REASSEMBLY IAW WGA ENGINEERING INSTRUCTIONS WITH A REPETITIVE INSPECTION INTERVAL OF 300 HOURS AND RETURNED RUB PLATE PEPLACEMENT INTERVAL OF 6 MONTHS REFERENCE EMAIL FROM N.WARE, WGA ENGINEERING DATED 18 APR 2025. TRNASFERRED TO LOG PAGE 224343 BTM M34 FO C/O PROCEDURES. C/O # 26762. AIRCRAFT APPROVED FOR RETURN TO SERVICE.