What was found
RIGHT MAIN LANDING GEAR WHEEL WELL AT FS 880 KEEL BEAM TO WEB ATTACH ANGLE WAS CORRODED. REMOVED SURFACE CORROSION IAW DC-8 SRM 51-1-8. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. FOUND BLEND OUT TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT MAIN LANDING GEAR WHEEL WELL AT FS 880 KEEL BEAM TO WEB ATTACH ANGLE WAS CORRODED. REMOVED SURFACE CORROSION IAW DC-8 SRM 51-1-8. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. FOUND BLEND OUT TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0.