- Owner type
- Co-owned, fractional ownership
- Serial number
- 6204
- Year built
- 2024
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 6, 2024
- Certificate issued
- August 31, 2026
- Expires
- August 31, 2033
- Mode S code
- A28B91
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 N263QSMatched 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 N263QSMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026080709146Indication Sys · malfunctionedCLIMBING THROUGH FL370 - FL390, POWER SWITCHED FROM CLB TO MCT ON ITS OWN. SHORTLY AFTER RECEIVED A LT ENG CAUTION & LT N2 WENT TO 0. ALL OTHER ENG PARAMETERS NORMAL. AFTER A COUPLE OF SECS, CAUTION DISAPPEAR & N2 WOULD RETURN TO NORMAL. IT DID THIS REPETEDLY SDR DXTA2026010906445Engine · vibrationWHILE IN CLIMB POWER AT FL310 THE LEFT ENGINE VIBRATION INDICATOR TURNED AMBER AND WAS INDICATING 3.1. AT COMPLETION OF THE CLIMB TO FL390 POWER WAS REDUCED TO 95.7 AND THE VIBRATION INDICATOR WAS STILL AMBER INDICATING 2.7. WHEN POWER WAS REDUCED TO 89.0 THSDR DXTA2025120105856Spring · brokenMAIN ENTRY DOOR T-HANDLE COVER RETURN SPRING IS BROKEN OR MISSING. GAINED ACCESS TO MED T-HANDLE COVER SPRING AND INSPECTED FOR ANY DEFECTS. FOUND SPRING UNSECURED, RE-1TACHED SPRING TO THE T-HANDLE COVER PIN. OPS CHECK IS GOOD, NO DEFECTS NOTED. WORK ACCOMPSDR DXTA2025110705555Pdu · defectiveREPEAT WRITE-UP. AT FL240 AND APPROXIMATELY 15 MINUTES FROMLAX WE GOT AN AMBER R REV UNLOCKED CAUTION EICAS MESSAGE AND ASSOCIATED EMER STOW UNLK SWITCH LIGHT. RAN THE QRH WITH CAUTION MESSAGES NOT EXTINGUISHING. PER THE QRH RIGHT ENGINE WAS SHUT DOWN AND WE SDR DXTA2025110705556Pdu · defectiveREPEAT WRITE-UP. AT FL240 AND APPROXIMATELY 15 MINUTES FROMLAX WE GOT AN AMBER R REV UNLOCKED CAUTION EICAS MESSAGE AND ASSOCIATED EMER STOW UNLK SWITCH LIGHT. RAN THE QRH WITH CAUTION MESSAGES NOT EXTINGUISHING. PER THE QRH RIGHT ENGINE WAS SHUT DOWN AND WE SDR DXTA2025101605302Switch · brokenAT 3000 FT, 10 MILES FROM TEB, AN AMBER R REV UNLOCKED APPEARED. WE RAN THE QRH, LIGHT DID NOT EXTINGUISH. AS PER THE QRH, WE SHUT DOWN THE RIGHT ENGINE AND DIVERTED TO EWR. CORRECTIVE ACTION: REMOVED THE DEFECTIVE RH T/R STOW MICRO SWITCH ANO INSTALLED A NEW SDR DXTA2025101305257Power Supply · defectiveTHE LIGHTS WERE FLASHING ALL OVER THE COCKPIT, AND LATER THERE WAS A BURNING ELECTRICAL SMELL. WE SHUT DOWN THE AIRPLANE QUICKLY. CORRECTIVE ACTION: GAINED ACCESS TO AIRCRAFT, REVIEWED FOOTAGE OF DISCREPANCY AND SPOKE WITH MCC ABOUT ISSUE. MCC STATED LIKELY TSDR DXTA2024100300721Door · lack of lubeMAIN DOOR: MAIN CABIN DOOR CANNOT BE OPENED FROM EXTERIOR. HANDLE POPS OUT BUT WILL NOT TURN. CORRECTIVE ACTION: LUBRICATED PASSENGER DOOR AND PERFORMED AN OPERATIONAL TEST WITH SATISFACTORY RESULTS. ALL WORK PERFORMED PER CL 300 AMM 12-20-04-640-807, 52-11-00SDR DXTA2024072912476Oven · failedAFTER OVEN TEMP WAS SET TO 325 DEGREES, SMOKE EMITTED INTO GALLEY AND COCKPIT. IT HAD AN ELECTRICAL SMELL. THE OVEN & EXHAUST FAN WERE TURNED OFF IMMEDIATELY AND THE SMOKE CLEARED. STARTED GAINED ACCESS TO ATTACH SCREWS, AFT DETENT SET SCREW IS SEIZED IN PANE
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.