What was found
CRACK ON RT UPPER AFT WINDOW RING PAN AT STA Y=1041, Y= 1098, Y=1117, Y=1193 AND 1212 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA487747-14MA, REV A, 493648-14 MA, REV A.