What was found
DURING HMV, FOUND LOWER FUSELAGE SKIN CORRODED AT FS 629-649 BETWEEN STRINGER 32 AND 34. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 FIG 825.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, FOUND LOWER FUSELAGE SKIN CORRODED AT FS 629-649 BETWEEN STRINGER 32 AND 34. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 FIG 825.