What was found
DENT ON FUSELAGE SKIN AT FWD SIDE OF FRAME 5, APPROX. 8" ABOVE S39-L. REPAIRED DAMAGE ON FUSELAGE SKIN FWD SIDE OF FRAME 5 APPROX. 8" ABOVE S39-L IAW A321 SRM 53-11-11-991-003. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT OF 60,000FC OR 120,000FH WHICHEVER COME FIRST. SUBSEQUENT INSPECTION INTERVALS AND INSPECTION METHOD TBD IS CASE OF AIRCRAFT LIFE EXTENSION MORE THAN 60,000FC/120,000 FH WHICHEVER OCCURS FIRST. APPLIED MONITOR DECAL IAW PROCESS STANDARD 900-5-1 NO. 4. (LP# 2038280)