What was found
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FUSELAGE SKIN DENTED, GOUGED AND CORRODED FROM FS 289 TO FS 588R, BETWEEN LONGERONS 18 AND 26R. REPLACED SKIN PANEL IAW DC-9 SRM 51-30-2, 51-30-5 AND ABX REA D953-13035-MR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FUSELAGE SKIN DENTED, GOUGED AND CORRODED FROM FS 289 TO FS 588R, BETWEEN LONGERONS 18 AND 26R. REPLACED SKIN PANEL IAW DC-9 SRM 51-30-2, 51-30-5 AND ABX REA D953-13035-MR.