- Owner type
- Co-owned, fractional ownership
- Serial number
- 6157
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 26, 2020
- Certificate issued
- October 23, 2025
- Expires
- October 31, 2032
- Mode S code
- A23C93
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 N243QSMatched 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 N243QSMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026012806693Water Separator · odorDIRTY SOCK ODOR OCCURRED DESCENDING THROUGH FL210 AND CONTINUED FOR THE REST OF THE FLIGHT. BOTH PACS ON N1 60% N2 77% ITT 450. ODOR IS SIGNIFICANT ENOUGH TO CAUSE EYE DISCOMFORT. CLEANED WATER SEPARATOR SOCK. OPS CHECK GOOD. IAW CL650 AMM 21-51-13-160-801SDR 3J7R2023071700001Bulb · blownDURING MAINTENANCE CHECKLIST FOUND EXTERNAL EMERGENCY LIGHT ON RH SIDE IS INOP (POS:FWD)SDR DXTA2022092871240None · noneWHEN CLOSING THE MAIN CABIN DOOR FROM INSIDE THE CABIN, THE HANDLE THAT IS PULLED TO BRING IN THE EXTERIOR HANDLE AND SEAL THE PRESSURE RELIEF FLAP IS VERY DIFFICULT TO PUSH BACK IN. // SIGNOFF// ADJUSTED THE SPRINGS ON THE HINGE ASSY AND RETURNED HINGE BACK ISDR DXTA2021082447610Handle · malfunctionedMAIN DOOR VENT DOOR: INTERIOR RED T HANDLE WILL NOT STOW. AMBER PAX DOOR STOW MESSAGE IS ILLUMINATED IN THE EICAS. EXTERIOR KEY LOCK NOW LOCKS IN THE REVERSE POSITION. EXTERIOR HORIZONTAL HANDLE WILL NOT EXTEND. LUBED DOOR HANDLE ASSEMBLY WITH NO DEFECTS NOSDR DXTA2021050341510Drive Shaft · stuckFLAPS FAIL AMBER CAS: AFTER TAKEOFF UPON SELECTING FLAP POSITION 0, FLAP FAIL CAS ILLUMINATED. FLAPS WERE STUCK BETWEEN 0 AND 20 DEGREES. QRC ACCOMPLISHED. REMOVED AND REPLACED ALL FLEXIBLE DRIVE SHAFTS ON RH/LH FLAPS. IAW CL-650 AMM 27-53-07-000-802. OPSDR DXTA2020120704441Brake Assy · defectiveON TAKE OFF, FLAPS FAILED TO RETRACT. THEY REMAINED IN THE FLAPS 20 SETTING. WE COMPLIED WITH THE FLAPS FAIL QRC AND RETURNED. POWERED UP AC. FLAPS ARE IN 20 DEG POSITION AS REBOOTED BY CREW. NO FLAP FAIL FAULT CURRENTLY DISPLAYED. CHECKED FAULT HISTORY.
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.