What was found
DURING INSPECTION, A CRACK WAS FOUND ON THE LT SILL AT STRINGER 3L & FRAME 20. THE SILL WAS REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, A CRACK WAS FOUND ON THE LT SILL AT STRINGER 3L & FRAME 20. THE SILL WAS REPLACED IAW SRM 51-40-02.