What was found
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT FS 1121, UPPER PORTION OF -17 FRAME BETWEEN LONGERON 29 LEFT TO 29 RIGHT. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10916-MR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT FS 1121, UPPER PORTION OF -17 FRAME BETWEEN LONGERON 29 LEFT TO 29 RIGHT. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10916-MR.