What was found
DURING A MAINTENANCE VISIT, FOUND PRESSURE PANEL CORRODED BEYOND LIMITATIONS, AT Y=920 AND X=+70. REMOVED CORROSION DAMAGE IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A MAINTENANCE VISIT, FOUND PRESSURE PANEL CORRODED BEYOND LIMITATIONS, AT Y=920 AND X=+70. REMOVED CORROSION DAMAGE IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R14.