As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN ANNUAL INSPECTION, A 0.300 INCH CRACK WAS FOUND IN THE FORWARD ATTACH SPAR (FUSELAGE) ANGLE AFT OF THE CHANNEL (P/N 20749-0). PIPER AD 75-12-06 REQUIRES INSPECTION OF THE BEND RELIEF HOLE IN THE CHANNEL AND STRAPS (PN 207 9-5 AND DASH 6). NO CRACKS WERE NOTED IN THESE PARTS. AIRCRAFT HAD NO RECORD OR INDICATIONS OF CRASH DAMAGE/GROUND DAMAGE. PART REPLACED WITH SERVICEABLE ANGLE.