What was found
(AUS) STAINLESS STEEL HYDRAULIC PIPE LOCATED IN THE RH ENGINE NACELLE AT THE REAR OF THE FIREWALL CRACKED AND LEAKING ON BEND RADIUS - TOTAL LOSS OF HYDRAULIC PRESSURE
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) STAINLESS STEEL HYDRAULIC PIPE LOCATED IN THE RH ENGINE NACELLE AT THE REAR OF THE FIREWALL CRACKED AND LEAKING ON BEND RADIUS - TOTAL LOSS OF HYDRAULIC PRESSURE