What was found
GSO - INSPECTION FOUND THE FUSELAGE SKIN BULGED OVER STRINGER 20L AT STA 970, BELOW REAR ENTRY. THE DAMAGED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-2 FIG 15 SRM 51-20-4 AND SRM 51-30-2. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND THE FUSELAGE SKIN BULGED OVER STRINGER 20L AT STA 970, BELOW REAR ENTRY. THE DAMAGED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-2 FIG 15 SRM 51-20-4 AND SRM 51-30-2. (W)