What was found
DURING CLIMBOUT, ON FLAP SLAT RETRACTION HAD TOTAL LOSS OF RIGHT SYSTEM HYDRAULIC PRESSURE AND FLUID. RETURNED TO DFW. FOUND LEAKING LINE AT RIGHT FWD FILTER MODULE IN TAIL COMAPARTMENT. REPLACED LINE OPERATION NORMAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CLIMBOUT, ON FLAP SLAT RETRACTION HAD TOTAL LOSS OF RIGHT SYSTEM HYDRAULIC PRESSURE AND FLUID. RETURNED TO DFW. FOUND LEAKING LINE AT RIGHT FWD FILTER MODULE IN TAIL COMAPARTMENT. REPLACED LINE OPERATION NORMAL.