What was found
DUE TO NUMBER ON HOLES FOUND ON INSPECTION, DOUBLER IS REQUIRED ON UPPER LEADING EDGE PER SRM 55-03-00 FIGURE 29. INSTALLED REPAIR DOUBLER TO UPPER LEADING EDGE PANEL PER SRM 55-03-00 AND SRM 51-60-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DUE TO NUMBER ON HOLES FOUND ON INSPECTION, DOUBLER IS REQUIRED ON UPPER LEADING EDGE PER SRM 55-03-00 FIGURE 29. INSTALLED REPAIR DOUBLER TO UPPER LEADING EDGE PANEL PER SRM 55-03-00 AND SRM 51-60-00.