What was found
(CAN) HYDRAULIC PRESSURE LINE NR 1 SYSTEM WORN THROUGH 1/2 WALL THICK AT LOCATION X124 LT NACELLE ABOVE EXHAUST. LINE WORN BECAUSE ADEL CLAMPS BROKE ALONG SIDE MLG RETRACTION ACTUATOR FITTER LOCATION AND RUBBED AGAINST LINE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) HYDRAULIC PRESSURE LINE NR 1 SYSTEM WORN THROUGH 1/2 WALL THICK AT LOCATION X124 LT NACELLE ABOVE EXHAUST. LINE WORN BECAUSE ADEL CLAMPS BROKE ALONG SIDE MLG RETRACTION ACTUATOR FITTER LOCATION AND RUBBED AGAINST LINE.