What was found
INITIAL INSPECTION: CRACK UPPER AFT CORNER ON WINDOW RING PAN RT STA Y= 1041. UPPER AFT CORNER ON WINDOW RING PAN RT STA Y= 1041 WAS REPAIRED PER SRM 53-05 FIG 122 AND ER/A 493648-14 MA REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INITIAL INSPECTION: CRACK UPPER AFT CORNER ON WINDOW RING PAN RT STA Y= 1041. UPPER AFT CORNER ON WINDOW RING PAN RT STA Y= 1041 WAS REPAIRED PER SRM 53-05 FIG 122 AND ER/A 493648-14 MA REV A.