- Owner type
- Co-owned, fractional ownership
- Serial number
- 6083
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 8, 2016
- Certificate issued
- June 22, 2026
- Expires
- June 30, 2033
- Mode S code
- A1F503
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 N225QSMatched 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 N225QSMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026071508812Warning System · malfunctionedREQUIRES MULTIPLE ATTEMPTS WHEN SHUTTING MAIN CABIN DOOR TO GET RED "PASSENGER DOOR" EICAS MSG TO EXTINGUISH, EVEN THOUGH ALL GREEN FLAGS ARE VISIBLE AND EXTERIOR HANDLE AND VENT FLAP ARE CONFIRMED FLUSH. PERFORMED OPERATIONAL TEST OF THE PASSENGER DOOR, OPSSDR DXTA2026030407103Latch Pin · lack of lubeMAIN PASSENGER DOOR, RED EICAS MESSAGE DISPLAYED. THE VISUAL TWO TOP GREEN LINES DO NOT LINE UP. PIC'S INCLUDED. ALSO NOTED, AOG MAIN CABIN DOOR NOT ALIGNING TO SHUT. CLEANED AND LUBRICATED THE LATCH PINS. COMPLIED WITH MUTIPLE MAINENTRANCE DOOR OPS CHECKSSDR DXTA2025090904888Rod · out of adjustWALKING UP TO THE AIRPLANE, NOTICED THE VENT DOOR WAS NOT FLUSH WITH CABIN DOOR. CANNOT COMPLY WITH MEL 52-70 WRITEUP, DOOR VENT WONT CLOSE COMPLETELY. TESTED CABIN DOOR TWICE WITH A CREWMEMBER ON BOTH SIDES OF DOOR TO ENSURE PROPER OPERATION, WITH AND WITHOUSDR DXTA2025052203570Door · faultedWHEN CLOSING THE MAIN CABIN DOOR NORMALLY THE UPPER TWO ROLLER LOCKS ARE NOT DISPLAYING MATCHING GREEN LINES. THE LINES ARE OFFSET BY A 1/4 OF AN INCH AND THE RED EICAS WARNING IS COMING ON AFTER ENGINE START. SLAMMING THE DOOR CLOSED AND PLAYING WITH THE HASDR DXTA2024010810528Wire Harness · damagedNLG: NOSE LANDING GEAR DID NOT EXTEND WHEN COMMANDED. THE TOWER REPORTED THE DOORS AS OPEN AND THE NOSE GEAR FULLY RETRACTED. WE ACCOMPLISHED THE GEAR DISAGREE CHECKLIST, GEAR 10-1. IT TOOK MULTIPLE RECYCLING ATTEMPTS FOR THE GEAR TO FINALLY DEPLOY AND SHOW GRSDR DXTA2023051786350Unknown · unknownFLAP ACTUATOR: DURING APPROACH WHEN FLAPS WERE SELECTED TO 30°, THEY REMAINED AT 20° , AND WE RECEIVE A "FLAP FAIL" AMBER CASS MESSAGE. AFTER PARKING ON THE RAMP, WE DISCOVERED THAT THE "FLAP MOTOR 1" CIRCUIT BREAKER WAS TRIPPED (BREAKER B 11 ON CB PANEL #3) SDR DXTA2023050185130Unknown · unknownMLG BRAKE PRESSURE: BRAKES SPONGY ON LANDING. THE RIGHT ONE SEEMS TO GRAB FIRST AND ALSO MAKE BRAKING UNEVEN. TECHS VERLFLED BOTH OR THE BRAKE ACUMULATORS WERE SERVICED PROPERLY. TECHS BLED THE #3 AND #4 BRAKE WITH A SMALL AMOUNT OF AIR NOTED. TECHS OPS CHECKSDR DXTA2021091548870Wire · defectiveDURING INITIAL CLIMB R 14TH DUCT CAS MESSAGE (RED) ANNUNCIATED. QRH CHECKLIST ACCOMPLISHED BUT CAS MESSAGE REMAINED ILLUMINATED. RETURNED TO DEPARTURE AIRPORT. COMPLIED WITH BOMBARDIER SMARTFIX TROUBLESHOOTING RECOMMENDATIONS. C/W STEP (23)&(38) AND FOUND DEFESDR DXTA2017121500001Apu · smokeSOURCE - OIR REPORT: ON TAKEOFF ROLL, SMOKE IN COCKPIT, ABORTED TAKEOFF AT UNKNOWN SPEED. CLEARED IT OUT. ANTI ICE FLUID IN API INTAKE IS ASSUMED. TOOK OFF W ENGINE PROVIDING AIR AND PRESSURIZATION WITH NO ANOMALIES. NO FURTHER ISSUES. (CREW NEVER CONTACTE
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.