As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOSS OF ALL A-SYSTEM HYDRAULIC FLUID DURING FLAP EXTENSION 0 DEGREES TO 2 DEGREES. ACCOPLISHED CHECK LIST LANDED NORMALLY. RII OB SEAL BLOWN NR 2 LE FLAP ACTUATOR. REMOVED AND REPLACED NR 2 LE FLAP ACTUATOR IAW MM CH 27-81-22. OPS CHECK AND LEAK CHECK GOOD.