- Owner type
- Co-owned, fractional ownership
- Serial number
- 6177
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 24, 2022
- Certificate issued
- August 24, 2026
- Expires
- August 31, 2033
- Mode S code
- A258ED
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 N250QSMatched 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 N250QSMatched 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 DXTA2025040702983Pneumatic System · faultedCOULD NOT DETERMINE SOURCE OF SMELL. STARTED WHEN WE SWITCHED TO ENGINE BLEED AFTER TAKEOFF. CONTINUED WHEN WE WENT BACK TO APU AIR. CORRECTIVE ACTION: RAN ENGINES AND APU FOR OVER 60 MINUTES AT IDLE AND HIGH-POWER. OPERATED AIR-CONDITIONING SYSTEM USING APU BSDR DXTA2025031902742Anti-Skid Sys · failedANTI SKID: UPON LANDING RUNWAY 5. ONCE THE GEAR WAS LOWERED THE ANTI-SKID FAILED ON BOTH CHANNELS. CORRECTIVE ACTION; TECHS WENT THROUGH THE AMM FOR THE OPS CHECK ON THE ANTISKID CONTROL ADJUSTMENT TEST CH.32-44-04 ( BITE TEST). AND ALL TESTS HAD PASSED.SDR DXTA2024121001405Overheat Loop · damagedL JETPIPE OVHT FAIL AMBER CAS: L JETPIPE OVHT FAIL AMBER CAS MESSAGE ILLUMINATED DURING LEVEL FLIGHT AT FL290. NO EMERGENCY DECLARED AND NO FURTHER ABNORMALITIES OBSERVED. PERFORMED APPROPRIATE CHECKLIST. REMOVED DEFECTIVE EXHAUST NOZZLE SENSING ELEMENT (PN:SDR DXTA2024092000578Steering Sys · false indicationNLG STEERING: DURING LANDING ROLL OUT, WE LOST NOSE WHEEL STEERING FOLLOWED BY A STEERING INOP CAS MESSAGE. PARKED A/C BY USING RUDDER PEDALS. PERFORMED NWS OPS CHECKS NOT CAS MESSAGE OR OTHER DEFECTS WERE NOTED,UNABLE TO DUPLICATE FAULT. ALL WORK WAS PERSDR DXTA2024080200072Warning Light · false activationRIGHT ANTI SKID LIGHT: DURING TAKEOFF ROLL "A/SKID OUTBD" ILLUMUNATED JUST PRIOR TO 80 KNOTS. DURING ABORT BRAKING PULLED TO THE RIGHT. PERFORMED OPS CHECK OF ANTISKID SYS IAW CL 650 AMM 32-44-00 OPS CHECK GOOD PERFORMEDBITE TEYS OF ANTISKID CONTROL SYS IAW CLSDR DXTA2024041711527Door · bindingMAIN CABIN DOOR IS EXTREMELY DIFFICULT TO OPEN FROM OUTSIDE AIRCRAFT. VERFIED MED HANDLE IS HARD/STIFF TO OPERATE FROM EXTERIOR ACCOMPLISHED GVI OF MED FRAME AND LOCKS AND NOTED UPPER MED TUBE LATCH PAWLS VERY STIFF CLEANED AND LUBERICATED AS REQUIRED IAW CL-SDR DXTA2023071090580Unknown · unknownMAIN DOOR HANDLE: WHEN YOU POP THE HANDLE ON THE MAIN ENTRY DOOR FROM THE OUTSIDE TO OPEN THE DOOR THE HANDLE POPS OUT BUT THEN ITS VERY DIFFICULT TO ROTATE THE HANDLE TO OPEN THE DOOR. YOU ACTUALLY HAVE TO MAKE AN EXTRA EFFORT TO PULL THE HANDLE OUT A LITTLE SDR DXTA2023061488750Unknown · unknownUNABLE TO OPEN DOOR FROM THE OUTSIDE.//CORRECITVE ACTION//CLEANED EXTERIOR MED HANDLE AND PERFORMED. OP TEST OF THE DOOR
WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW 52-11-00. NO DEFECTS NOTED.
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.