What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE HOLE A (CONFIRM INDICATION USING BOROSCOPE) IN PASSENGER CABIN (2 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00032) REF AE WO 2024-413/1. N/R# 2024 - 749159. PERFORMED REPAIR ON HOLE A LOC. FRAME 20RH JOGGLE AREA AT LEVEL STOP FITTING 7 IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CONSIDERED PSE IAW A320 SRM 51-11-12. THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 8,900FC(FH NO RELEVANT)SUBSEQUENT INSPECTION INTERVALS UNTIL 60,000FC (FH NOT RELEVANT ) IS 5,900FC(FH NOT RELEVANT) INSPECTION METHOD FOR LEADER HOLE REFER TO SRM 53-11-12-300-012. FIG 14 INSPECTION METHOD FOR ASSOCIATED HOLE PER SRM 53-11-12-300-012. FIG 13. ACCOMPLISHED BY AE TECH# 8623721. AE QC# 174. FUR-A320-53-01932 ASSIGNED.