What was found
CRACK ON LT UPPER AFT WINDOW RING PAN AT STA Y=1041, Y=1079, Y=1193, Y=1212, Y=1231, AND Y=1250 AT CABIN FUSELAGE STRUCTURE. RING PAN 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.