- Owner type
- Co-owned
- Serial number
- 6066
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 25, 2016
- Certificate issued
- July 2, 2026
- Expires
- July 31, 2033
- Mode S code
- A1C25F
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 129
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1982 | 6 |
| 1984 | 1 |
| 1988 | 1 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 1 |
| 1994 | 5 |
| 1995 | 5 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 3 |
| 2000 | 5 |
| 2001 | 7 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 2 |
| 2005 | 5 |
| 2006 | 6 |
| 2007 | 6 |
| 2008 | 2 |
| 2009 | 5 |
| 2010 | 9 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 5 |
| 2017 | 8 |
| 2018 | 4 |
| 2019 | 5 |
| 2020 | 2 |
| 2021 | 4 |
| 2022 | 7 |
| 2023 | 8 |
| 2024 | 6 |
| 2025 | 3 |
| 2026 | 4 |
Airframe · Bombardier CL-600-2B16
AD 2026-14-09Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-07-01Landing gearInformation bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Bombardier CL-600-2B16
SAIB AIR-21-15R1Navigation SystemSAIB NM-11-51Ice and Rain Protection: Wing Anti-Ice SystemSAIB NM-10-13Navigation: Flight Management SystemSAIB NE-03-28Engine · GE CF34-3B
SAIB NE-04-77Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N212QSMatched 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 Bombardier CL-600-2B16 aircraft
FAA incident reports
No FAA accident or incident reports matched to N212QSMatched 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 Bombardier CL-600-2B16 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026033007300Unknown · odorWHILE ON VISUAL APPROACH CAVU DAY WE HAD THE SMELL OF SMOKE THROUGH THE AIRPLANE. WE COULD NOT IDENTIFY THE SOURCE. PERFORMED A BREAKAWAY TORQUE CHECK OF THE LEFT AND RIGHT ACM TURBINES IAW AMM PART II TASK 21-51-00-720-801. BREAKAWAY TORQUE WITHIN LIMITS ATSDR DXTA2025102705423Selector Valve · faultedWHILE APPROACHING THE AIRPORT WE GOT A RED CAS GEAR DISAGREE MESSAGE AND A MOMENTARY RED CAS NOSE DOOR OPEN MESSAGE THAT WENT OUT WHILE RUNNING THE GEAR DISAGREE CHECKLIST. HAD UP INDICATIONS FOR THE 3 GEAR. WHILE RUNNING THE QRH FOR GEAR DISAGREE GOT TO WHERSDR DXTA2025100305160Acm · damagedPUNGENT ODOR IN ENTIRE ACFT AFTER TURNING PACKS ON WITH APU RUNNING. ODOR DID NOT IMPROVE OVER TIME. EVEN WITH MAIN DOOR & CARGO DOORS OPEN, ODOR REMAINS STRONG & WAS IRRITATING TO NOSTRILS. REPEAT WRITE UP. REMOVED LT & RT WATER SEPARATORS & PERFORMED LT & SDR DXTA2025071404204Engine · vibrationIN FLIGHT, AT CRUISE, THE RIGHT ENGINE AMBER VIBRATION DISPAYED AT 2.7. PER QRH, AFTER PULLING BACK POWER, VIBRATION INDICATOR REDUCED BACK TO GREEN BUT AT AN ELEVATED READING OF 2.5 TO 2.6. A SLIGHTLY SLOWER CRUISE SPEED WAS REQUIRED TO KEEP INDICATOR IN SDR DXTA2025060503738Brake · faultedON POST FLIGHT NOTICED THE INBOARD BRAKE ON THE RIGHT MLG WAS SMOKING AND EXTREMELY HOT. WE WERE VERY LIGHT ON LANDING AND DID NOT USE ANY ABNORMAL BRAKING. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR BRAKE ASSEMBLY WITH OVERHAULED. REPLACED BRAKE BOSDR DXTA2025051003436Selector Valve · faultedURING OCF FOR GEAR DISAGREE, AFTER THE 1ST COMPLETE CYCLE OF THE LANDING GEAR THE NOSE LANDING GEAR DID NOT EXTEND. WE DECLARED AN EMERGENCY, AND PROC ENDED TO OUR ALTERNATE AIRPORT KACT. WE PROCEEDED TO RUN QRH PROCEDURE 10-17 MANUAL GEAR EXTENSION. THE MAIN SDR DXTA2025042203153Landing Gear · warning messageGEAR DISAGREE RED CAS: DURING LANDING WHEN GEAR WAS SELECTED DOWN BOTH MAIN GEAR SHOWED GREEN DN AND NOSE GEAR SHOWED A WHITE UP. AFTER A FEW SECONDS WE HAD A RED GEAR DISAGREE CAS. CREW DID A GO AROUND AFTER CLEANING UP THE PLANE CREW REQUEATED VECTORS FORSDR DXTA2024102300906Control Unit · faultedANTI SKID: GETTING READY TO TAXI FOR DEPARTURE WITH ENGINES RUNNING NO ANTISKID LIGHT SOON AS PARKING BRAKE WAS RELEASED BOTH THE ANTISKID INBOARD AND OUTBOARD LIGHT ILLUMINTED SEVERAL ATTEMPTS WITH SETTING AND RELEASING PARKING BRAKE RESULTED IN THE AMBSDR DXTA2023111610067Unknown · unknownSELECTING LDG GEAR DOWN RESULTED IN A RED GEAR DISAGREE CAS LIGHT & AUDIBLE 'GEAR DISAGREE' OVER THE SPEAKER. IT WAS NLG POSITION THAT WAS NOT DOWN & LOCKED. NLG WAS ACTUALLY DOWN, BUT NLG DOORS WERE OPEN DUE TO THE LOUD WINDSTREAM NOISE. GEAR DISAGREE QRH CSDR DXTA2023061288220Unknown · unknownR JETPIPE OVHT RED CAS: DURING LEVEL FLIGHT AT 40,000' THE RIGHT JETPIPE OVERHEAT CAS MESSAGE ILLUMINATED. CREW PERFORMED JETPIPR OVRHT QRC CHECKLIST. CAS MESSAGE WENT AWAY AS WE RETARDED / REDUCED THE RIGHT POWER LEVER/ THRUST LEVER. PRIOR TO FLIGHT FIRE MOSDR DXTA2018060741023Transmitter · faultedLEVEL AT FL380, FLAP DISPLAY ILLUMINATED AND INDICATED BETWEEN 2 AND 3 DEGREES. THE F/A CONFIRMED THAT THE FLAPS APPEARED TO BE EXTENDED SLIGHTLY. A FEW MINUTES LATER FELT THE FLAPS MOVE AND THEY INDICATED 5 DEGREES. THE AUTO THROTTLES FAILED AND NEVER RE-ENSDR DXTA201806041023Flap System · malfunctionedAT FL380, FLAP DISPLAY CAME ON AND INDICATED BETWEEN 2 AND 3 DEGREES. THE F/A CONFIRMED THAT THE FLAPS APPEARED TO BE EXTENDED SLIGHTLY. A FEW MINUTES LATER, FELT THE FLAPS MOVE AND THEY INDICATED 5 DEGREES. THE AUTO THROTTLES FAILED AND NEVER REENGAGED. HY
STCs that may be installed · 857
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bombardier CL-600-2B16
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 ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.