As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING GROUND PRESSURIZATION RUN FOR T/S. VISUAL INSPECTION FOUND 12 INCH CRACK IN UPPER WHEEL WELL PRESSURE SKIN ALONG AIRCRAFT CENTER LINE AT EDGE OF STRINGER BETWEEN FRAMES 29 TO FRAME 32. AIRCRAFT WAS PREVIOUSLY SUBJECT TO A COMPANY SPECIAL INSPECTION FOR THIS PROBLEM ON OTHER SIMILAR AIRCRAFT IN OPERATORS FLEET ON MAY 24/2003 AND NO REPORTED DISCREPANCIES FOUND. AIRCRAFT REPAIRED AS PER BAE REPAIR INSTRUCTION HC532H9018. AIRCRAFT RETURNED TO SERVICE.