- Owner type
- Co-owned, fractional ownership
- Serial number
- 6129
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- September 30, 2025
- Expires
- September 30, 2032
- Mode S code
- A227A7
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 120
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 | 1 |
| 2000 | 4 |
| 2001 | 4 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 4 |
| 2007 | 3 |
| 2008 | 2 |
| 2009 | 4 |
| 2010 | 6 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 5 |
| 2017 | 8 |
| 2018 | 4 |
| 2019 | 5 |
| 2020 | 1 |
| 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 · 4
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N238QSMatched 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 N238QSMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026051508060Air Filter · dirtyWHEN TURNING APU BLEEDS ON, YOU GET A STRONG DIRTY SOCK SMELL FROM THE AIR. IT DISSIPATED WHEN USING ENGINE BLEEDS BUT CAME BACK ONCE WE WENT BACK TO APU BLEEDS. IT IS STRONGER ON THE GROUND VS INFLIGHT. CORRECTIVE ACTION: REMOVED BOTH L/H AND R/H FILTER SOCSDR DXTA2025092205025Oil System · leakingSTRONG SMELL OF OIL COMING FROM THE OVERHEAD VENTS. WE RAN THE APU FOR 45 MINUTES WITH NO CHANGE. REPEAT WRITEUP. REMOVED APU DUE TO INTERNAL OIL LEAK AND REPLACED WITH AN INSPECTED APU. PERFORMED SYSTEM OPERATION AND LEAK CHECK, NO DEFECTS NOTED. SYSTEM LSDR DXTA2025070104078Oxygen Mask · unwanted deployDURING DESCENT INTO KBZN CABIN LOST PRESSURIZATION AND PASSENGER OXYGEN MASKS DROPPED.AT APPROXIMATELY 11000FT ON APPROACH TO KBZN CABIN LOST PRESSURIZATION. CABIN CLIMBED TO 10000FT THEN DESCENDED TO 8500FT THEN CLIMBED AGAIN AND DESCENDED BACK TO APPROXIMATESDR DXTA2025052203555Seal Rest · leakingCLIMBING THROUGH 9000FT THE AMBER CABIN ALT CAS MESSAGE DISPLAYED FOLLOWED BY A LOUD HISSING NOISE THAT SEEMED TO BE FROM THE MAIN CABIN DOOR. REPLACE PAX DOOR SUPPORT HOUSING ASSY. AND DOOR SUPPORT STRUT PER MM 52-11-25. LEAK CHECK GOOD.SDR DXTA2025010801822Seal · leakingDECENDING INTO TQPF WE EXPERIENCED LOSS OF PRIMARY DOOR SEAL ON MAIN CABIN DOOR. RESECURED BONDING JUMPER. OPS CHECK GOOD. IAW CL650 AMM 52-11-28SDR DXTA2024090300369Wire · looseCABIN EMERG LIGHT: THE MIDDLE EMERGENCY ARRIOW LIGHT UNDER THE DIVAN IS INOPERATIVE. CORRECTIVE ACTION: FOUND LOOSE LOAD WIRE ON DIVAN ARROW CONNECTOR. RESECURED WIRE AS REQUIRED . OPS CHECK GOOD NO DEFECTS AT THIS TIME. WORK PERFORMED IN REFERENCE TO CL-650 ASDR DXTA2023092796590Unknown · unknownEMERG EXIT SIGN/LIGHT: EMER EXIT SIGN ABOVE SEAT #1 IS INOP. ALL OTHER EMERGENCY LIGHTS IN CABIN ARE FUNCTIONAL. //SIGNOFF// FOUND EMERGENCY LIGHT LED PANEL CONNECTOR NOT FULLY PLUGGED IN. RECONNECTED CONNECTOR IAW CHALLENGER 650 SPM 20-20-00. OPS CHECK OF LH SDR DXTA2021082347500Unknown · odorAFTER TAKEOFF, A BURNING ODOR IN ACFT. (NON ELECTRICAL) F/A FIRST NOTICED. COCKPIT INDICATORS NORMAL, NO OUTSIDE PARAMATERS. FLIGHT ONLY LASTED 10 MINS W/ODOR WHOLE FLT. NO LINGERING ODORS OBSERVED. GAINED ACCESS TO APU & PERFORMED GIV OF APU AND BOX. NO
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.