What was found
RIGHT NR 8 SLAT COVE PANEL INNER SKIN IS CHAFED AT OUTBOARD RIB XOS 1185. BLENDED OUT CHAFED AREA IAW SRM 57-00-00-2R FOUND TO BE OUT OF LIMITS, PERFORMED A DOUBLER REPAIR IAW SRM 57-40-01-2R AND EA 1-5750-T0330795.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT NR 8 SLAT COVE PANEL INNER SKIN IS CHAFED AT OUTBOARD RIB XOS 1185. BLENDED OUT CHAFED AREA IAW SRM 57-00-00-2R FOUND TO BE OUT OF LIMITS, PERFORMED A DOUBLER REPAIR IAW SRM 57-40-01-2R AND EA 1-5750-T0330795.