What was found
DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE FUSELAGE RH CENTER WING BOX PRESSURE PANEL ATTACHMENT HOLE B BETWEEN FR 35& FR 36. NOTE: NO INDICATIONS WERE FOUND ON THE L/H SIDE OF THE PRESSURE PANEL. THE SUBJECT HOLE WAS REAMED TO REMOVE THE DAMAGE AND AIRBUS WAS CONTACTED. AIRBUS PROVIDED REF. /5/ TD, HAECO ACCOMPLISHED THE TD WITHOUT DEVIATION AND REQUESTED RDAS. REF. /2/ RDAS WAS PROVIDED. EC A19-336-01 IS ISSUED TO ACCOMPLISH THE PERMANENT REPAIR AS REF. /1/REO WITHOUT DEVIATIONS. EC A19-336-02 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTION OF THE SB CUT OUT AREA AS PER REF. /2/ RDAS. EC A19-336-03 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTION OF THE HOLES OUTSIDE SB REINFORCEMENT AS PER REF. /2/ RDAS; THIS REPAIR IS APPROVED AS PER REF. /2/ RDAS. THIS IS A CATEGORY B REPAIR AND IS CLASSIFIED AS MAJOR.