What was found
PDX - C5 CHECK. LT INBOARD FLAP UPPER SKIN CHAFED. REMOVED RIVETS FROM AREA AND BLENDED OUT DAMAGE. DAMAGE AFTER BLENDING WAS BEYOND LIMITS. PERFORMED REPAIR IAW R/D 8/4-57-1194 STEPS 6&7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX - C5 CHECK. LT INBOARD FLAP UPPER SKIN CHAFED. REMOVED RIVETS FROM AREA AND BLENDED OUT DAMAGE. DAMAGE AFTER BLENDING WAS BEYOND LIMITS. PERFORMED REPAIR IAW R/D 8/4-57-1194 STEPS 6&7.