- Owner type
- Co-owned, fractional ownership
- Serial number
- 6182
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 2, 2022
- Certificate issued
- December 3, 2025
- Expires
- December 31, 2032
- Mode S code
- A26412
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 N253QSMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Reports on N253QS not matched to an aircraft · 1
They name N253QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another 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 DXTA2026091409670Seal · leakingDURING CLIMB AND DESCENT BELOW 10000 FT WE CAN HEAR LOUD WIND/SUCTION NOISE COMING FROM MAIN CABIN DOOR. CABIN DIF/RATE SHOWED NORMAL VALUES. VERIFIED CREW SQUAWK. TECHS REMOVED FAULTY MAIN CABIN DOOR SEAL AND REPLACED WITH CUSTOMER PROVIDED NEW ASSY. IAW AMMSDR DXTA2026080609121Smoke Detector · defectiveRED CAS SMOKE TOILET LIGHT STAYED ON DURING FLGHT NO SMOKE OR FUMES DETECTED CORRECTIVE ACTION: REPLACED SMOKE DETECTOR. OPS CHECK GOOD. IAW CL650 SMM 26-14-01SDR DXTA2026070908711Control Panel · faultedIMMEDIATELY AFTER TAKEOFF, NOTICED AIRCRAFT WAS NOT PRESSURIZING IN AUTO MODE. CLIMBED TO 5000' AND RAN MANUAL PRESSURIZATION QRH WITH NEGATIVE RESULTS. REMOVED AND REPLACED CABIN PRESSURIZATION PANEL WITH A NEW CUSTOMER SUPPLIED UNIT, OPS CHECK SATISFACTORY.SDR DXTA2026040907560Selector · faultedON DEPARTURE, AIRCRAFT FAILED TO PRESSURIZE. NO CONTROL OF PRESSURIZATION VIA AUTO OR MANUAL. DURING CLIMB AND DECENT HEARD AIR RUSHING NOISE FROM MAIN CABIN DOOR. AFTER LANDING NOTICED VENT DOOR FLAP LOOSE ON MAIN CABIN DOOR. REMOVED NEW SEAL IAW MM 52-11-2SDR DXTA2026021006816Push-Pull Rod · defectiveTHE MAN DOOR SUPPORT (FOOT) IS INOP. ALLOWING THE DOOR TO COME IN CONTACT WITH AND REST ON THE RAMP WHEN OPENED. REMOVED DAMAGED DOOR SUPPORT PUSH PULL ROD IAW AMM 52-11-25 VERIFIED AREA OK FOR INSTALLATION. ADJUSTED REPLACED PUSHROD TO 15.470 +0 -. 018. SDR DXTA2025062003966Seal · failedDEPARTED KSGR AND CABIN ALT WAS CLIMBING AT THE SAME RATE AS THE AIRPLANE. ONCE THE APU WAS SHUTDOWN, THE CABIN RATE INCREASED MORE. WE LEVELED OFF AT 9000 FT, CABIN ALT READ 9000 FT , ALSO. IN THE DESCENT, THE CABIN DOOR STARTED MAKING A LOUD HISSING NOISE ANSDR DXTA2025061903922Seal · leakingON TAKEOFF CABIN PRESSURIZATION WAS CLIMBING WITH THE AIRCRAFT. CABIN ALTITUDE MATCHED ALTIMETER AND VERTICAL SPEED INDICATOR AS WE CLIMBED TO 4000 FT. LOUD NOISE WAS HEARD ON MAIN CABIN DOOR INFLIGHT AT 200 KTS. PERFORMED OPS TEST OF THE PRESSURIZATION SYSTESDR DXTA2024092200597Outflow Valve · slowCABIN PRESSURIZATION CONTROL: DURING OUR INITIAL CLIMB, SHORTLY AFTER TAKEOFF, WE NOTICED THAT OUR CABIN PRESSURE WAS CLIMBING AT THE SAME RATE AS OUR AIRPLANE WAS CLIMBING, 3600+' PER MINUTE. THE CABIN ALTITUDE CONTROL WAS SET FOR OUR DESTINATION OF 4900 FEETSDR DXTA2023062689290Unknown · unknownMAIN DOOR: MAIN CABIN DOOR MECHANICAL STOP AFT PAD BROKEN OFF AT ATTACH POINT. REMOVED AND REPLACED AFT MED MECHANICAL STOP WITH CUSTOMER SUPPLIED STOP. STOP PN 600-38090-3 AND DOWEL PIN PN 600-38090-5. OPS CHECK GOOD AT THIS TIME. AMM 52-11-00-720-801.
Reports on N253QS not matched to an aircraft · 17
They name N253QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2017050300001Plate · corrodedDURING EVALUATION OF CORROSION ON TCAS BONDING PLATE (WHICH IS ATTACHED TO PANEL 170AB) FOUND PLATE TO BE OUT OF ACCEPTABLE LIMITS. REMOVED TCAS PLATE PER SRM 51-40-03. MANUFACTURED NEW TCAS PLATE IAW DWG F2MA285033C01SDR DXTA2016050506234Relay · failedWITHIN 5 MINUTES AFTER TAKEOFF AN ELEC BURNING RUBBER SMELL BECAME NOTICEABLE. SOURCE & LOCATION NOT DETECTABLE. ODOR SMELL MOST NOTICEABLE IN COCKPIT & SLIGHTLY NOTICEABLE IN CABIN. OPERATED WINDSHIELD HEAT & NOTICED THE LT WINDSHIELD HEAT WAS NOT WORKING SDR DXTA2016050406232Unknown · odorTHE SMELL OF BURNING RUBBER FILLED THE ACFT DESCENDING OUT OF 8000 FT. THE FLIGHT ATTENDANT THOUGHT THE SMELL WAS WORST WHEN GEAR WENT DOWN, ALSO THE TOP LEAD PAX RT CONTROL PANEL WAS VERY HOT. RAN APU & OPERATED AIR CONDITIONING SYS FULL HOT & FULL COLD WIT
See all 17 unmatched reportsSTCs 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.