What was found
DURING 'C' CHECK, MAINTENANCE FOUND FUSELAGE UPPER SKIN LAP CORRODED BEYOND LIMITS AT STRINGER 10L BS 1325. INSTALLED REPAIR IAW 53-30-3, FIGURE 14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 'C' CHECK, MAINTENANCE FOUND FUSELAGE UPPER SKIN LAP CORRODED BEYOND LIMITS AT STRINGER 10L BS 1325. INSTALLED REPAIR IAW 53-30-3, FIGURE 14.