What was found
(AUS) FLAP SYSTEM HYDRAULIC PIPE CHAFING ON MARMON CLAMP. PIPE IS LOCATED FORWARD OF THE MAIN SPAR INBOARD OF THE WING/FUSELAGE JOIN ADJACENT TO AIR CONDITIONING DUCTS. PART TC: 8,860.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) FLAP SYSTEM HYDRAULIC PIPE CHAFING ON MARMON CLAMP. PIPE IS LOCATED FORWARD OF THE MAIN SPAR INBOARD OF THE WING/FUSELAGE JOIN ADJACENT TO AIR CONDITIONING DUCTS. PART TC: 8,860.