What was found
RIGHT MAIN LANDING GEAR WHEEL WELL HAD CORROSION ON INBOARD UPPER CHAMBER ON TRAP FITTING. BLENDED AND REMOVED CORROSION FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0, FIGURE 1, SHEET 3. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT MAIN LANDING GEAR WHEEL WELL HAD CORROSION ON INBOARD UPPER CHAMBER ON TRAP FITTING. BLENDED AND REMOVED CORROSION FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0, FIGURE 1, SHEET 3. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.