What was found
REPAIRED FUSELAGE SKIN BLEND OUT 1.6 INCHES ABOVE STRINGER S-23L, STA: BS 926.5 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48, PAGES 256 TO 260 AND 264, DETAIL VII, PAGES 261 AND 281 AND 51-70, FIGURE 1, PAGE 4, 51-30-2, PAGE 3C AND 51-30-3, PAGE 7. REFERENCE NON-ROUTINE TASK CARD 737 AND 514, DATED MARCH 18, 2010.