As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER TAKE OFF DURING RETRACTION, THE INBOARD FLAPS REMAINED AT 2 DEGREES (SPLIT FLAP CONDITION). WHILE FOLLOWING THE CHECK LIST WE LOST SYSTEM A HYDRAULICS. PERFORM SYSTEM A LOSS CHECKLIST AND LANDED UNEVENTFULLY. LANDED HARD (FIRM). REMOVED AND REPLACED INBOARD FLAP DRIVE HYDRAULIC MOTOR. OPERATIONAL CHECK AND LEAK CHECKED GOOD PER 27-50 MAINTENANCE MANUAL. VISUAL INSPECTION FOR HARD LANDING. NO DEFECTS NOTED. OK FOR SERVICE.