What was found
INSPECTION FOUND INTERIOR CRACKS ON VERTICAL FIN LEADING EDGE FORWARD OF PITOT TUBE AROUND COUNTER SINK. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND INTERIOR CRACKS ON VERTICAL FIN LEADING EDGE FORWARD OF PITOT TUBE AROUND COUNTER SINK. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.