- Owner type
- Co-owned, fractional ownership
- Serial number
- 6169
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 30, 2021
- Certificate issued
- July 29, 2025
- Expires
- July 31, 2032
- Mode S code
- A24401
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 N245QSMatched 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 N245QSMatched 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 DXTA2026061608430Seal · leakingMAIN DOOR WAS MAKING A LOUD NOISES ON APPROACH INTO MORRISTOWN. PASSENGERS AND FLIGHT ATTENDANT NOTICE IT. NO NOISE ON TAKEOFF. REMOVED MAIN CABIN ENTRY DOOR SEAL & INSTALLED NEW MAIN CABIN ENTRY DOOR SEAL IAW CL350 52-11-28. ALL OPS AND LEAK CHECKS GOOD.SDR DXTA2026031307214Warning Message · false activationON TAXI OUT WE GOT THE AMBER A/SKID INBD CAS MESSAGE.2). ON TAXI OUT WE GOT THE AMBER A/SKID OUTBD CAS MESSAGE. DOWNLOADED FAULT HISTORY AND SENT TO NETJETS MX CONTROL. C/W THE OPERATIONAL TEST OF THE ANTISKID SYSTEM. OPS CHECK GOOD IAW AMM 32-44-00. C/W THESDR DXTA2025123106320Cover · unsecureFOAM DOOR HINGE COVER HAD BECOME UNVELCROED AND GOT STUCK IN DOOR DURING CLOSING. DOOR WAS LOWERED AND AND PIECE OF FOAM WAS REMOVED. DOOR CLOSED NORMALLY. ON DEPARTURE, HEARD LOUD HISS FROM DOOR SEAL AND PRESSURIZATION WAS NOT ON SCHEDULE. STAYED AT 10000' ANSDR DXTA2025050103283Lamp · inoperativeDURING SHC FOUND THAT THE RH AFT MOST EMERGENCY LIGHT INOP CORRECTIVE ACTION: THE REMOVAL AND INSTALLATION OF THE R/H MOST AFT EMERGECCY LAMP ASSY AS REQ'D. IAW: CL 650 MM 33-51-04. OPS CHECK GOOD. THIS CLEARS MELSDR DXTA2024072912473Seal · leakingDURING DEPARTURE CLIMB FA NOTIFIED THE CREW THAT A LOUD HISSING SOUND WAS AN EMANATING FROM THE MAIN CABIN DOOR. PILOT INSPECTED THE DOOR AND HEARD THE SAME SOUND ON THE LEFT SIDE OF THE MAIN CABIN DOOR. THIS NOISE WAS LOUDER THAN NORMAL INFLIGHT AMBIENT SLIPSSDR DXTA2024060311952Handle · malfunctionedDURING DOOR CLOSING SEQUENCE, THE DOOR HANDLE PLUNGER OPERATES AND STOWS NORMALLY. AFTER 2-3 SECONDS, THE EXTERIOR DOOR HANDLE POPS OUT AND RED UNLOCK FLAG ON DOOR APPEARS. AMBER PAX DOOR OUT HANDLE CAS MESSAGE POSTED. AFTER THIS WAS PUT THROUGH THE CREW EISDR DXTA2023011678580Spinner · looseDURRING TAKEOFF, A NOTICEABLE HUM & VIBRATION. LEFT ENGINE VIB INDICATOR SHOWED 2.3. DURRING THE CLIMB, THE VIB INDICATOR CONTINUED TO CLIMB. PASSING 38250' THE INDICATOR REACHED 2.7, & TURNED AMBER. RETURNED TO FL380. WITH SUBSEQUENT POWER REDUCTION, THE VIBSDR DXTA2022112274520Apu · overheatedUPON APPROACH INTO AIRPORT AFTER START ATTEMPT OF APU, WE OBSERVED AN APU RED CAS MESSAGE OF APU LOW OIL PRESSURE FOLLOWED BY RED CAS MESSAGE OF APU OVER TEMP. THIS FOLLOWED BY AN AUTO SHUTDOWN. REMOVED APU, INSTALLED REPAIRED APU. SERVICED WITH 2.5 QTS OF
Reports on N245QS not matched to an aircraft · 14
They name N245QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR EBVR20180403001Skin · corrodedTWO SPOTS OF BLENDED CORROSION ON TOP SIDE OF L/H WING REQUIRES NDT AND POSSIBLE SUBMITTAL TO FALCON JET.
AFTER BLENDING AND NDT THE TWO BLENDS WERE MAPPED AND SUBMITTED TO FALCONJET ENGINEERING FOR REVIEW. FALCONJET
ENGINEERING DIVIDED THE SUBMITTAL INTO TWSDR DXTA2016020306178Display · inoperativeIMMEDIATELY AFTER ROTATION ON TAKEOFF, BOTH THE PILOT SIDE PFD & MFD WENT BLACK. TWO SECONDS LATER, SMOKE BEGAN TO RISE FROM IN FRONT OF THE GLARE SHIELD. THE COPILOT PFD HAD ALL RED FLAGS. NO CBS WERE POPPED & BOTH GENERATORS REMAINED ONLINE. PERFORMED ANSDR DXTA2015060906026Probe · out of limitsWINDSHIELD XFR LIGHT CAME ON INFLIGHT & SMOKE ODOR. TROUBLE SHOT & FOUND L512DG WAS NOT RECEIVING POWER. FOUND WINDOW PROBE TO BE OUT OF LIMITS, HIGH RESISTANCE. REMOVED DEFECTIVE PILOT WINDSHIELD 10SA & INSTALLED A NEW PILOT WINDSHIELD 10SA. PERFORMED ALL
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.