What was found
CRACK ON LONGERON 8LT BS 1296 AT INNER FUSELAGE STRUCTURE. LONGERON SECTION DAMAGE WAS REMOVED AND NEW LONGERON SECTION WAS INSTALLED IAW SRM 53-02, FIG 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LONGERON 8LT BS 1296 AT INNER FUSELAGE STRUCTURE. LONGERON SECTION DAMAGE WAS REMOVED AND NEW LONGERON SECTION WAS INSTALLED IAW SRM 53-02, FIG 18.