What was found
CRACK ON LT LOWER AFT WINDOW RING PAN AT STA Y=598 AND Y=826 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT LOWER AFT WINDOW RING PAN AT STA Y=598 AND Y=826 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.