What was found
FRAME AT Y=1440 AND LONGERON 33R CORROSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED FRAME BY INSTALLING A SPLICE REPAIR IAW REO-01936 AND TREATED AREA DC-8 IAW SRM 51-1-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME AT Y=1440 AND LONGERON 33R CORROSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED FRAME BY INSTALLING A SPLICE REPAIR IAW REO-01936 AND TREATED AREA DC-8 IAW SRM 51-1-8.