What was found
DURING INSPECTION, A DAMAGE WAS FOUND COMMONT TO A TOOL HOLE OF BULKHEAD AT STA1140, S-18R TO S-19R. AND NO ALLOWANCE DAMAGE LIMIT WAS PROVIDED IN SRM. A REPAIR THAT BLENDED OUT THE DAMAGED FRAME WEB AT A TOOLING HOLE AND REFINISHED THE SURFACE PER BOEING MESSAGE NUMBER TEC-SOF-11-0035. THE DEVIATION WAS APPROVED UNDER BOEING SERVICE REQUEST 1-1972007720 ON ODA-300064-NM FAA FORM 8100-9 DATED SEPTEMBER 15, 2011. A NEW FAA APPROVAL WHICH CONTAINS THE INSPECTION REQUIREMENTS MUST BE ISSUED PRIOR TO THE INSPECTION THRESHOLD OF 35000 FLIGHT CYCLES.