This N-number isn't registered right now. Below is its last known registration, canceled Dec 21, 2018.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2017)5 ADs may apply2 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 student pilot’s improper landing flare and subsequent failure to maintain directional control during the landing roll.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA17CA516)
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 (DA 40 NG) |
| 2022-13-06 | Cargo Compartments | Aug 11, 2022 | Airframe (DA 40 NG)Only with: Includes Model DA 40 D airplanes that have been converted to Model DA 40 NG airplanes. |
| 2016-23-03 | Turbocharging | Nov 29, 2016 | Airframe (DA 40 NG) |
| 2016-22-06 | Autopilot | Nov 16, 2016 | Airframe (DA 40 NG)Certain serial numbers: DA 40 NG 40.N260–40.N314; DA 42 NG 42.N150–42.N223; DA 42 M-NG 42.MN035–42.MN052 |
| 2013-08-21 | Turbocharging | May 21, 2013 | Airframe (DA 40 NG)Certain serial numbers: DA 40 NG 40.N001–40.N084. Only with: Also applies to all serial numbers of Model DA 40 NG airplanes converted from Model DA 40 D. |
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.
WING FUEL CAP INTERNAL BLACK PLASTIC RIB BREAKS OFF INSIDE THE LOWER FUEL CAP RETAINER ASSEMBLY.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A ROUTINE 100 HR INSPECTION, THE TECH DISCOVERED THAT THE ROLL SERVO BRIDLE CLAMP WAS CRACKED BUT STILL ATTACHED TO THE RT AILERON CONTROL ROD. THE TECH REPLACED THE CLAMP.
From FAA Service Difficulty Reports; matched by N-number and serial number.