As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT,THE FUSELAGE RT SIDE WINDOW FRAME (50R) AT STA 1155 TO 1174 WAS DAMAGED AND CORRODED LOWER SIDE. BLENDED PER SRM 53-05, FIG 111 SHEET 2 NOTE 12 PAGE 502. ACCOMP NDT INSP USING HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS WERE FOUND. REPAIRED PER DRAWING SRO 9530053 AND ARA 16486A.