What was found
DURING RAMP INSPECTION, FOUND CRACK IN TOP SKIN JUST OUTBOARD OF OUTBOARD HINGE POINT. CRACK ALIGNED WITH CRACK IN SKIN P/N 96-610006-3. SUB-SURFACE STRUCTURE SHOWED NO DAMAGE, BUT CRACKED PAINT IN BALANCE WEIGHT ATTACH AREA INDICATES PREVIOUS STRESS. AIRCRAFT TOTAL TIME, 4,524 HOURS.