What was found
LOSS OF LEFT HYDRAULIC QUANTITY LEVEL DECREASED TO 1.8 WITH ASSOCIATED SYSTEM PRESSURE LIGHT ILLUMINATION. LEFT MAIN DOWNLOCK ACTUATOR HYDRAULIC LINE RUPTURED. REPLACED HYDRAULIC LINE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOSS OF LEFT HYDRAULIC QUANTITY LEVEL DECREASED TO 1.8 WITH ASSOCIATED SYSTEM PRESSURE LIGHT ILLUMINATION. LEFT MAIN DOWNLOCK ACTUATOR HYDRAULIC LINE RUPTURED. REPLACED HYDRAULIC LINE.