What was found
SEVERE CORROSION OF LIFT STRUT ATTACH FITTING. FRONT OF FRONT SPAR IN RIGHT WING LOCATED UNDER LEADING EDGE COVERING CAUSED BY LACK OF ACCESS FOR INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SEVERE CORROSION OF LIFT STRUT ATTACH FITTING. FRONT OF FRONT SPAR IN RIGHT WING LOCATED UNDER LEADING EDGE COVERING CAUSED BY LACK OF ACCESS FOR INSPECTION.