What was found
DURING ROUTINE C CHECK INSPECTION, FOUND FLAP MECHANISM OF INNER WING FORWARD LINK CRACKED AT STATION 3.000 RIGHT. REMOVED REPLACED INNER WING FORWARD LINK OF FLAP MECHANISM IAW OHM 27-27-1 PAGE 4. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. GOOD IAW DC8 MAINTENANCE MANUAL 27-11-0 PAGE 10-14, DC8 27-21-0 PAGE 5-9. DC8 27-30-0 PAGE 4-7, DC8 27-40-0 PAGE 1-2 DC8 27-41-0 PAGE 10-13, DC8 27-51-0 PAGE 11-12, DC8 27-61-0 PAGE 5-7, DC8 27-70-0 PAGE 1-2 DC8 27-80-0 PAGE 4.