What was found
INTERNAL SKIN AT Y=1050 AND Y=1060 BETWEEN LONGERONS 35R AND35L CORROSION PAST LIMITATIONS. REPAIRED INTERNAL SKIN BY DOUBLER AND FILLER REPAIR IAW REO-01934 AND TREATED AREA IAW DC-8 SRM 51-1-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL SKIN AT Y=1050 AND Y=1060 BETWEEN LONGERONS 35R AND35L CORROSION PAST LIMITATIONS. REPAIRED INTERNAL SKIN BY DOUBLER AND FILLER REPAIR IAW REO-01934 AND TREATED AREA IAW DC-8 SRM 51-1-8.