As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) WIRING LOOM LOCATED IN FLAP RECESS INBOARD OF THE LT ENGINE WAS CHAFED AND BADLY BURNT. TWO POWER WIRES FOR THE LT STANDBY HYDRAULIC PUMP AND ONE POWER WIRE FOR THE RT STANDBY HYDRAULIC PUMP OPEN CIRCUITED. WIRE 7611-10006D22-2 (ECU WIRING) WAS ALSO OPEN CIRCUITED. OTHER WIRES IN THE LOOM WERE CHAFED OR HEAT AFFECTED.