What was found
REPAIRED FUSELAGE SKIN BLEND OUT AT STRINGER S-23L, STA: BS 897 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MAR 10, 2010, SECTION 53-30-1, FIGURE 1 AND 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 206, DATED MAR 08, 2010.