What was found
DURING HEAVY MAINTENANCE, SECONDARY FINDING ELONGATED HOLE CUT OUT FUEL TANK ACCESS PANEL 640KB ON RT WING (HOLE 2) FOR TRACKING PURPOSE ONLY; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00044 ) REF AEROMAN WO 2026-252/1 NR 2026-355336 PERFORMED PERMANENT REPAIR ON (HOLE NR 2) LOCATED ON BOTTOM SKIN PANEL NR 2 BTW RIB 15 TO RIB 16 AT RT WING, THIS REPAIR IS CATEGORY B, INSTALLED BOLTS P/N NAS1790-5R13 ON ACCESS PANEL 640KB IAW SRMA320 SRM 57-21-11-300-002, FOR BUSHING INSTALLED ON HOLE NR 2 INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT AS FOLLOWING 1000FC/42000FH AND SUBSEQUENT INSPECTION AT INTERVALS OF 4800FC/9600FH,METHOD OF INSPECTION GVI IAW SRM A320 57-21-11-205-036 TABLE 3. THE REPAIR PROCEDURE IS DOCUMENTED IN 2026-355187. FUR A320-57-03413