As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO COMPRESSION CRACKS ON RIGHT WING REAR SPAR, ONE ON EITHER SIDE OF PLYWOOD DOUBLER AT STRUT ATTACH POINT. OUT BOARD CRACK EXTENDS APPROX ONE THIRD DEPTH OF SPAR, EXTENT OF INBOARD CRACK AS YET UNKNOWN, MAY GO BEHIND DOUBLER, CRACKS FOUND DURING INSPECTION REQUIRED BY AD 2000-25-02.