What was found
DURING INSPECTION, FOUND ONE CRACK COMMON TO FRAME AT STA 654+121, BETWEEN S-9R AND S-10R. ONE CRACK COMMON TO FRAME AT STA 654+121, BETWEEN S-9R AND S-10R ACCOMPLISHED REPAIR IAW PRI 583789-14 REV.0 AND PRI 583789-14 REV.1, COMPARED AND COMPLIED WITH ER/A 583789-14 REV. ORIGINAL SECTION I, NO DEVIATION. FOR FURTHER, ACCOMPLISH ER/A 583789-14 REV. ORIGINAL SECTION II INSPECTION BEFORE A/C REACHES THE THRESHOLD OF 30,000 TOTAL FLIGHT CYCLES, REFER TO LOG PAGE:1411240.