What was found
DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FWD FUSELAGE SKIN CRACKED THROUGH RIVET HEAD AT LT JACK PAD AREA FS 191 WL 180L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 191 WL 180 LBL 61.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FWD FUSELAGE SKIN CRACKED THROUGH RIVET HEAD AT LT JACK PAD AREA FS 191 WL 180L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 191 WL 180 LBL 61.