- Registered owner
- 412 Jw Aviation LLC
- Location
- Dover, DE
- Owner type
- LLC
- Serial number
- 304
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Experimental, research and development
- Airworthiness date
- August 23, 2016
- Certificate issued
- September 25, 2017
- Expires
- September 30, 2027
- Mode S code
- A7DD99
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 41
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1983 | 1 |
|---|---|
| 1984 | 1 |
| 1986 | 1 |
| 1987 | 7 |
| 1988 | 1 |
| 1989 | 6 |
| 1991 | 1 |
| 1992 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 5 |
| 1999 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2014 | 1 |
| 2015 | 1 |
| 2017 | 2 |
| 2018 | 1 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
Airframe · C A S A C-212-CD
AD 2022-17-06FuselageAD 2020-03-18Flight ControlsAD 2018-19-02Flight controlsInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N606ARMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on C A S A C-212-CD aircraft
FAA incident reports
No FAA accident or incident reports matched to N606ARMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on C A S A C-212-CD aircraft
Service difficulty reports · 18
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 39LA20150404133Nut · out of positionTHE 2 ENG POWER LEVER HAD NO CONTROL OVER THE ENG DURING CRUISE FLIGHT. THE NR 2 ENG WAS SHUTDOWN IN FLIGHT & AN EMER WAS DECLARED. THE ACFT LANDED WITHOUT INCIDENT. INSPECTED NR 2 ENG CONTROL SYS & FOUND THAT THE NUT FOR THE PROPELLER PITCH CONTROL INPUT LSDR 39LA2013072400164Bracket · corrodedFOUND CENTER WING RT OTBD FLAP BRACKET, INBD AND OTBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKINS PN'S 212-13202-05-1 AND 212-13202-05-2. REPAIR PREFORMED IAW EO2012032-309 AND EO2021032-424, AND DWG NR 2012032-2032.SDR 39LA2013072400154Skin · dentedTWO DENTS FOUND ON LOWER SURFACE OF RT WING AT APPROX WING STATION 9350. REPLACED WING SKIN IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG N R 2012032-2033.
See all 18 reportsSTCs that may be installed · 37
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · C A S A C-212-CD
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST04105NYInstallation of Flight Data Recorder, Flight Data Acquisition Unit, Traffic Advisory Altering System and Navigation SuiteSTC ST04109NYUpdate of COMBI