What was found
DURING PREFLIGHT, FOUND CRACK 18.5 INCHES LONG IN COMPOSITE PANEL LOCATED IN THE LOWER REAR BODY GEAR/WING TRAILING EDGE FILLET. CRACK IS DIRECTLY BEHIND THE LOWER WATER DRAIN ACCESS HATCH, IN THE LEFT OF THE AIRCRAFT CENTERLINE, BEHIND THE LEFT BODY GEAR, NEAR AND PARALLEL TO WHERE IT JOINS THE FUSELAGE SKIN. REPAIRED PANEL AS PER ENGINEERING DRAWING B4 - 06125.