What was found
COMBINED HYDRAULIC SYSTEM FLUID LOSS DUE TO FITTING BECOMING LOOSE AT FLIGHT POWER SHUTOFF VALVE. SECURED FITTING, SERVICED AND TESTED SYSTEM, SUBSEQUENT OPERATION NORMAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COMBINED HYDRAULIC SYSTEM FLUID LOSS DUE TO FITTING BECOMING LOOSE AT FLIGHT POWER SHUTOFF VALVE. SECURED FITTING, SERVICED AND TESTED SYSTEM, SUBSEQUENT OPERATION NORMAL.