What was found
(CAN) FUEL LEAK AT #2 ENGINE. RIGID FUEL TUBE PUNCTURED BEHIND CLAMP AT REAR SECTION BETWEEN FS 1975 AND 1860 OVER WL200. LINE REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) FUEL LEAK AT #2 ENGINE. RIGID FUEL TUBE PUNCTURED BEHIND CLAMP AT REAR SECTION BETWEEN FS 1975 AND 1860 OVER WL200. LINE REPLACED.