This N-number isn't registered right now. Below is its last known registration, canceled Jun 29, 2017.
Safety record in brief:1 NTSB accident (destroyed damage, Jul 2016)9 ADs may apply5 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 pilot's exceedance of the airplane's critical angle of attack while maneuvering in turbulence and gusty wind conditions, which resulted in an aerodynamic stall/spin.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR16FA144)
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 |
|---|---|---|---|
| 2026-06-03 | Hoses and tubes | Apr 30, 2026 | Airframe (DA40 F) |
| 2024-19-08 | Nose/Tail Landing Gear | Nov 29, 2024 | Airframe (DA40 F) |
| 2022-13-06 | Cargo Compartments | Aug 11, 2022 | Airframe (DA40 F)Only with: Includes Model DA 40 D airplanes that have been converted to Model DA 40 NG airplanes. |
| 2014-13-08 | Wings | Aug 27, 2014 | Airframe (DA40 F)Certain serial numbers: DA 40 40.006–40.009; DA 40 40.011–40.1071; DA 40 40.1073–40.1077; DA 40 F 40.FC001–40.FC029 |
| 2010-25-01 | Diamond Aircraft Industries GmbH Models DA 40 and DA 40F Airplanes | Jan 11, 2011 | Airframe (DA40 F) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2009-07-14 | Diamond Aircraft Industries GmbH Model DA 40 and DA 40F Airplanes | May 11, 2009 | Airframe (DA40 F)Certain serial numbers: DA 40 40.377; DA 40 40.420; DA 40 40.422; DA 40 40.644–40.693; DA 40 40.695–40.842; DA 40 40.844; … |
| 2006-10-21 | Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods | Jun 22, 2006 | Engine (O-360-A4M)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004. |
| 2006-06-16 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and… | Apr 27, 2006 | Engine (O-360-A4M)Only with: Engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (O-360-A4M)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
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.
DISTRIBUTOR ARM COMING LOOSE FORM THE GEAR. WHEN THE ARM COMES LOOSE, IT CAUSES WEAR ON THE ARM CTR AND AS THE CTR WEARS TO A LARGER DIAMETER HOLE, THE ARM FLIES OUT CLOSING THE GAP AND GRINDS INTO THE CONTACTS OF THE DISTRIBUTOR BLOCK. THE MAG RAN NORMAL AND WAS FOUND DURING AN INSPECTION.
From FAA Service Difficulty Reports; matched by N-number and serial number.FWD DOOR LATCH ASSY BUSHINGS WORKED LOOSE. FAILURE OF LOCKING FLUID WHICH HOLDS THE BUSHINGS IN PLACE. USE OF A DIFFERENT METHOD TO SECURE BUSHINGS IN HINGE ASSY FOR PERHAPS A SIMPLER ASSY WITH FEWER MOVING PARTS.
From FAA Service Difficulty Reports; matched by N-number and serial number.UPON 100 HR INSP, AFT DOOR, FWD HINGE WAS FOUND TO BE CRACKED RESULTING IN REMOVAL OF DOOR FROM SERVICE AND SENDING OUT FOR REPAIR. THIS IS EITHER THE RESULTS OF THE DOOR PROP STRUT BEING TOO STRONG OR THE DOOR BEING LEFT OPEN AND CATCHING A GUST OF WIND. CONSTRUCTION OF HINGE USING A STRONGER…
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER 2.5 HOURS OF FLIGHT TIME, AFTER SINGLE TOUCH AND GO AND DURING CLIMB OUT, THE PILOT NOTICED THE REAR DOOR WARNING LIGHT AND TRIED TO RE-ENGAGE PRIMARY DOOR LATCH. THIS RESULTED IN AN IN-FLIGHT SEPARATION AND SUBSEQUENT LOSS OF DOOR ASSEMBLY. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER A PREVIOUS FLIGHT AND BEFORE THE NEXT STUDENTS FLIGHT, THE ELECTRIC FUEL PUMP WAS FOUND TO BE INOPERATIVE. INADEQUATE COOLING IS WHAT WE BELIEVE TO BE THE SOURCE OF THE MALFUNCTIONS. PROVIDE RAM AIR FOR PROPER COOLING OF FUEL PUMP AND MOTOR. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.