What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 TO 380, STRINGER 20R TO 22R. THE DENTED AREA OF SKIN WAS CUT OUT AND NEW SKIN, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 AND 9, SRM 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 TO 380, STRINGER 20R TO 22R. THE DENTED AREA OF SKIN WAS CUT OUT AND NEW SKIN, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 AND 9, SRM 51-10-2 AND 51-30-2.