What was found
REPAIRED DAMAGED STRINGER TO BELT FRAME CLIP AT STA BS 986.5, STR S24L BY REPLACEMENT WITH NEW P/N 69-35364U2 IN ACCORDANCE WITH BOEING STRUCTURAL REPAIR MANUAL (SRM), CHAPTER 51-30-02, PARAGRAPH 7, PAGE 5, AND BOEING DRAWING 65-46548, REV DD, DATED JUNE 15, 1999. REFERENCE KELOWNA FLIGHTCRAFT NON-ROUTINE TASK 247, DATED JULY 22, 2009.