This N-number isn't registered right now. Below is its last known registration, canceled Nov 1, 2019.
Safety record in brief:1 NTSB accident (substantial damage, Jul 2019)No ADs since 1998 matched3 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The airplane's floats impact with an ocean wave or swell, which exceeded the design load specifications of the flying wire assemblies and resulted in a partial separation of the float assemblies.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for ANC19FA035)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
FORWARD LT LOWER TIE-ROD (FLYING WIRE) WIRE-PULL ATTACHMENT FAILED. THE AFT RT UPPER TIE-ROD (FLYING WIRE) WIRE-PULL ATTACHMENT FAILED. THE AIRCRAFT'S RIGIDITY TO ITS FLOATS BECAME EFFECTED, THE AIRCRAFT PIVOTED (ROLLED) TO THE LEFT. THE AIRCRAFT'S LT WING CONTACTED THE WATER RESULTING IN IT…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE CYLINDER HEAD SEPARATED FROM THE BARREL ON CYLINDER NR 9.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT ELEVATOR TIP RIB WAS FOUND PERFORATED BY CORROSION UNDER MASS BALANCE WEIGHTS C2TE-113 AND DASH 115. ONLY ONE FASTENER WAS RETAINING THE WEIGHTS. THE LEAD WEIGHTS ARE ON BOTH SIDES OF THE ALUMINUM RIB AND ARE RETAINED BY STEEL SCREWS. THE CONDITIONS ARE PERFECT FOR CORROSION.
From FAA Service Difficulty Reports; matched by N-number and serial number.