As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE C/W AD CF 92-26, A CRACK WAS DISCOVERED VISUALLY IN THE LOWER FORWARD SPAR CAP. A SECOND CRACK APPROXIMATELY 1.1250 INCH WAS FOUND IN THE RADIUS OF SHEAR ANGLE. INSPECTION WAS C/W PRE AD REQUIREMENT. AD CALLS FOR ULTRASONIC TESTING.