What was found
FUSELAGE SKIN HAS A DENT ON THE PREVIOUS REPAIR FASTENER AT BS 500D+10'; 2' BELOW S-R7. REPAIRED FUSELAGE SKIN DISCREPANCY AREA OF BS 500D+10'; 2' BELOW STR 7R, IAW SRM.53-00-01-2R-3 88302U 05OCT20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS A DENT ON THE PREVIOUS REPAIR FASTENER AT BS 500D+10'; 2' BELOW S-R7. REPAIRED FUSELAGE SKIN DISCREPANCY AREA OF BS 500D+10'; 2' BELOW STR 7R, IAW SRM.53-00-01-2R-3 88302U 05OCT20.