As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) UPPER CAP ANGLE FOUND BROKEN AND A CRACK HAD DEVELOPED IN THE MAIN PANEL. CRACK APPROX 2 INCHES TO 2.50 INCHES IN FRONT OF P/N 204-060-651-001, TUBE ASSY AND EXTENDING 10 INCHES VERTICAL DOWN AND DISAPPEARS BEHIND THE OWER CAP ANGLE. THE CRACK ALSO EXTENDS UPWARDS BEHIND THE ANGLE BETWEEN THE MAIN PANEL AND FORWARD BULKHEAD. AIRCRAFT TT: 14,959 HOURS.