What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294 BETWEEN LONGERON 24 AND 25L AND AT STA 225, L16L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294 BETWEEN LONGERON 24 AND 25L AND AT STA 225, L16L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-02.