What was found
EXTERNAL FUSELAGE BETWEEN BS 520 AND BS 540, BETWEEN STR 29L AND STR 28L HAS A DENT. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT THE DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER AND INSTALLED PER TIMCO REO 2 0284. PER UAL EVA 81196, THE FUSELAGE SKIN REPAIR BETWEEN BS 525 - BS-555, AND STR 26L AND 28L HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH 085625 ONLY, AND A NEW FAA 8100-9 MUST BE ISSUED AND DTA INFORMATION INCORPORATED IN THE AIRPLANE MAINTENANCE PROGRAM BEFORE 08AUG2013. THE AIRCRAFT WILL BECOME UNAIRWORTHY IF A NEW FAA 8100-9 IS NOT ISSUED ON OR BEFORE 08AUG2013.