As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE CRACK STA 426, STR 4L,11"LONG. MAJOR REPAIR ACCOMPLISHED: REPAIRED IAW EVA 80084. REPAIR IS APPROVED FOR STATIC STRENGTH. A NEW 8100-9 MUST BE ISSUED PRIOR TO SEP 17 2012 OR A-C WILL BECOME UNAIRWORTHY. THIS REPAIR APPROVED FOR STATIC STRENGTH. COMPLIANCE TO 14CFR 26.43(D) AND 25.571 IS DF'D FOR PERIOD NOT TO EXCEED 24 MONTHS FROM 9-17-2010. A NEW 8100-9 MUST BE ISSUED FINDING COMPLIANCE.