What was found
DEFORMATION IN FUSELAGE SKIN AT BS 1460 TO 1480, S32L TO S34L. DAMAGED AREA SMOOTHED AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 53-30-01 LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DEFORMATION IN FUSELAGE SKIN AT BS 1460 TO 1480, S32L TO S34L. DAMAGED AREA SMOOTHED AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 53-30-01 LIMITS.