What was found
CRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 RT, CARD 14, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14 AD REV ORIGINAL. LENGTH CRACK 0.150". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REV WITH AMOC IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER 24 MONTHS FROM REPAIR ACCOMPLISHMENT. DAMAGE TOLERANCE ANALYSIS AND A NEW AMOC IS REQUIRED IAW PROCEDURES ESTABLISHED BY ADVISORY CIRCULAR 120-43 UNDER LOG 2634653. AMOC APPROVAL TO AD 2007-11-13 IS REQUIRED FOR SERVICE BEYOND 60,000 TOTAL FLIGHT CYCLES.