What was found
DURING D CHECK INSPECTION, FOUND CORROSION ON FRAME AT F/S 200 LONGERON 36. REMOVED CORROSION, FABICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20D, 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D CHECK INSPECTION, FOUND CORROSION ON FRAME AT F/S 200 LONGERON 36. REMOVED CORROSION, FABICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20D, 51-1-21.