What was found
(CAN) LEAKING FOUND AT SWAGED FITTING ON HYDRAULIC MANIFOLD END. SIGNIFICANT FLUID LOSS. FOUND ON POST FLIGHT INSPECTION. FLUID SLIGHTLY BELOW MIN LEVEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) LEAKING FOUND AT SWAGED FITTING ON HYDRAULIC MANIFOLD END. SIGNIFICANT FLUID LOSS. FOUND ON POST FLIGHT INSPECTION. FLUID SLIGHTLY BELOW MIN LEVEL.