What was found
FUSELAGE SKIN EXTERIOR SURFACE CHAFED AT FR33-4" STR40 RT SIDE LOCATION. BLENDED OUT AND SMOOTHED CHAFING AREA IAW SRM 51-74-10. EXCEED LIMIT IAW SRM 53-10-12-101. PERFORMED DOUBLER REPAIR IAW SRM 53-10-12/201, FIG 208.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN EXTERIOR SURFACE CHAFED AT FR33-4" STR40 RT SIDE LOCATION. BLENDED OUT AND SMOOTHED CHAFING AREA IAW SRM 51-74-10. EXCEED LIMIT IAW SRM 53-10-12-101. PERFORMED DOUBLER REPAIR IAW SRM 53-10-12/201, FIG 208.