This N-number isn't registered right now. Below is its last known registration, canceled Mar 15, 2026.
Safety record in brief:1 NTSB accident (substantial damage, May 2023)10 ADs may apply8 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 failure of the ferry fuel tank system to transfer fuel during a trans-Pacific flight for reasons that could not be determined, which resulted in fuel starvation and a subsequent ditching into the water.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR23LA192)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2022-11-12 | Engine Controls | Jul 13, 2022 | Airframe (DHC-6-400)Certain serial numbers: 001–989 |
| 2022-11-09 | Wing Structure | Jul 6, 2022 | Airframe (DHC-6-400) |
| 2022-10-03 | Flight Control System | Jun 23, 2022 | Airframe (DHC-6-400)Certain serial numbers: 001–987 |
| 2022-10-07 | Flight Control System | Jun 23, 2022 | Airframe (DHC-6-400) |
| 2022-08-13 | Turbine Section | May 27, 2022 | Engine (PT6A-34) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2022-07-14 | Aircraft Fuel System | May 13, 2022 | Airframe (DHC-6-400)Certain serial numbers: DHC-6-400 845–957 |
| 2022-03-04 | Time Limits | Mar 17, 2022 | Airframe (DHC-6-400) |
| 2019-10-05 | Flight Controls | Jun 20, 2019 | Airframe (DHC-6-400) |
| 2018-04-02 | Flight Controls | Mar 27, 2018 | Airframe (DHC-6-400) |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-34)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
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.
THE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF THE TUBE IN THE QUADRANT NOTED BY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF THE TUBE IN THE QUADRANT NOTED BY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF THE TUBE IN THE QUADRANT NOTED BY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF THE TUBE IN THE QUADRANT NOTED BY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE QUADRANT ON RUDDER TORQUE TUBE WAS FOUND TO HAVE MOVEMENT BETWEEN THE TUBE AND THE QUADRANT. UPON LAST INSTALLATION A INDEX LINE WAS PLACED ON THE TUBE AND QUADRANT. WITH THE GUST LOCK ON AND THE RUDDER PEDALS MOVED BY AN INDIVIDUAL THERE WAS MOVEMENT OF THE TUBE IN THE QUADRANT NOTED BY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER TAKE OFF, AT 300 FT, THE NR 2 PROPELLER AUTOFEATHERED, THE AUTOFEATHER WAS SELECTED OFF AND THE PROPELLER UNFEATHERED AND RETURNED TO NORMAL OPS. TORQUE WAS OBSERVED BY THE CREW DURING THE AUTOFEATHER AND THE THROTTLE WAS RETARDED TO PREVENT AN OVER TORQUE. NR 2 AUTOFEATHER PRESSURE SWITCH…
From FAA Service Difficulty Reports; matched by N-number and serial number.RUDDER TORQUE TUBE, BELL CRANK ATTACHMENT RIVETS AND BELL CRANK SHOWING SIGNS OF BEING LOOSE. ATTACH RIVETS ARE SMOKING.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE ACFT FITTED WITH AMPHIB FLOATS HAD A NOSE GEAR FAILURE PREVIOUSLY AT 344.5 HRS. INITIAL FINDINGS OF THE FAILURE WERE THOUGHT TO BE FROM INTERGRANULAR CORROSION. NEW PARTS WERE FITTED AT THAT TIME. AT AFTT 422.6, JULY 2, 2015 THE NOSE GEARS WERE REMOVED AS AN INTERNAL COMPANY INSPECTION TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.