As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING TAKEOFF ROLL (80 KNTS), HYDRAULIC ''C'' SYSTEM LOST ALL FLUID. A/C RETURN TO GATE. INVESTIGATION FOUND LOWER FLANGE OF LT MLG ACTUATOR CRACKED AT END CAP AND THE PISTON TRAVELLED OUT OF THE CYLINDER.CYLINDER ASSEMBLY REPLACED, HYDRAULIC SYSTEM REPLENISHED, AIRCRAFT RELEASED.LOCKHEED SB 93-32-238 ALREADY ADDRESSES THE OCCURRENCE WITH THE REPLACEMENT OF THE ACTUATORS WITH A -109. OPERATOR ALREADY IN UPGRADE PROGRAM.