As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING COMPLIANCE OF AD 00-25-02 R1, HAIR-LINE CRACKS WERE FOUND AT WING STRUT ATTACH POINT ON BOTH LT AND RT FWD WING SPARS. APPROXIMATELY THREE INCHES OF LONGITUDINAL CRACK WAS FOUND OTBD AND INBD OF PLYWOOD DOUBLERS. NO COMPRESSION CRACKS NOTED. THE ACFT OWNER DECIDED TO HAVE NEW METAL SPAR WINGS MFG AND INSTALLED.