What was found
DURING A/C CONVERSION FOUND CORROSION ON INNER CHORD OF FRAME STA 1263 BETWEEN S-17R TO 18R, BLENDED AREA BY 1.460" X 0.780" AFTER CORROSION CLEANUP FOUND MINIMUM THICKNESS BY 0.014" AND ORIGINAL THICKNESS IS 0.100"
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A/C CONVERSION FOUND CORROSION ON INNER CHORD OF FRAME STA 1263 BETWEEN S-17R TO 18R, BLENDED AREA BY 1.460" X 0.780" AFTER CORROSION CLEANUP FOUND MINIMUM THICKNESS BY 0.014" AND ORIGINAL THICKNESS IS 0.100"