What was found
ON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER THE TITANIUM STRAP AT FRAME 21, BETWEEN STRINGERS 19L AND 20L. THE SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER THE TITANIUM STRAP AT FRAME 21, BETWEEN STRINGERS 19L AND 20L. THE SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 202.