What was found
DURING HEAVY MAINTENANCE, SECONDARY FINDING ELONGATED HOLE CUT OUT FUEL TANK ACCESS PANEL 640KB ON RT WING ; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00042 ) REF AEROMAN PERFORMED PERMANENT REPAIR ON (HOLE #1) LOCATED ON BOTTOM SKIN PANEL #2 BTW RIB 15 TO RIB 16 AT RH WING, THIS REPAIR IS CATEGORY B, INSTALLED BOLTS P/N NAS1790-5R13 ON ACCESS PANEL 640KB IAW SRM A320 SRM 57-21-11-300-002, FOR BUSHING INSTALLED ON HOLE #1 INSPECTION THRESHOLD FROM AIRCRAFT FIRSTFLIGHT AS FOLLOWING 24400FC/48800FH AND SUBSEQUENT INSPECTION AT INTERVALS OF 4800FC/9600FH, METHOD OF INSPECTION GVI IAW SRM A320 57-21-11-205-036 TABLE 3. THE INSPECTION METHOD TO TRACKING ONLY HOLE #2 IS DOCUMENTED IN 2026-355336. HOLE #1 FUR-A320-57-03412