- Owner type
- Co-owned, fractional ownership
- Serial number
- 6062
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 26, 2016
- Certificate issued
- August 3, 2026
- Expires
- August 31, 2033
- Mode S code
- A1DC60
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 N219QSMatched 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 N219QSMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026081209220Controller · faultyA SKID OTBD AMBER CASS MESSAGE CAME ON DURING LANDING PHASE. RAN QRH, DIVERTED TO KBED. REMOVED AND REPLACED ANTI-SKID CONTROLLER IAW AMM 32-44-04. OPS CHKS FOUND NORMAL.SDR DXTA2025021402355Door · unknownMAIN DOOR: WE WERE UNABLE TO CLOSE THE MAIN CABIN DOOR WE HAD CAS MESSAGE -PAXDOOR OUT HNDL AND GREEN INDICATIONS NOT ALIGN. CORRECTIVE ACTION: OPERATIONAL CHECKS COULD NOT DUPLICATE THE DISCREPANCY. OPS CHECK GOOD. IAW CL650 AMM 52-11-00.SDR DXTA2024021610919Bolt · shearedMAIN CABIN DOOR CUTOUT FORWARD STOP BRACKET BOLT HAS SHEARED OFF. PART LOCARED IN LEFT PILOT CUP HOLDER. REMOVED UPPER FWD BROKEN STOB BOLT & DOWEL PIN, INSPECTED STOP BOLT ATTACHED FITTING NO DEFECTS NOTED, INSTALLED CUSTOMER SUPPLIED NEW STOP BOLT PN: 600-SDR DXTA2024012210688Cable · malfunctionedIN FLIGHT, AT 5000 FEET FROM KPNE TO KTEB, FLIGHT ATTENDANT CAME FORWARD, SAYING THE CABIN DOOR WAS MAKING A LOT MORE NOISE THAN NORMAL. WHEN I WAS ABLE, I WENT TO THE BACK AND LOOKED AT IT AND WE NOTICED THAT ONE OF THE DOOR CABLES HAD NOT RETRACTED FULLY INTSDR DXTA2024010310501Power Supply · faultyAT FL380 WE HAD AN UNCOMMANDED FLAP EXTENSION. IT STARTED AT 2 PERCENT AND VERY SLOWLY, OVER ABOUT 15 MINUTES, EXTENDED TO 20 PERCENT. WE DIVERTED AND DESCENDED TO FL240 WHERE THE FLAPS ABRUPTLY RETRACTED. THE FLAPS THEN SLOWLY FLUCTUATED BETWEEN 9 PERCENT SDR DXTA2023072891860Unknown · unknownEMERGENCY LIGHTS ON STATUS MESSAGE ON EICAS INTERMITTANT THROUGH OUT FLIGHT. EMERGENERY LIGHTS SWITCH WAS IN ARM POSITION & THE EMERGENCY LIGHTS DID NOT ILLUNATE IN CABIN WHEN EMERGENCY LIGHTS STATUS MSG CAME ON. SELECTING EMERGENCY LIGHTS ON AT THE SWITCH. SDR DXTA2023062289150Unknown · unknownMAIN DOOR: MAIN ENTRY DOOR HAS VERY LOUD AIR NOISE COMING INTO GALLEY AREA. ON INTERIOR RIGHT SIDE (2 OCLOCK) OF DOOR FRAME A GAP IS VISIBLE TO THE OUTSIDE AT CRUISE FLIGHT. ///SIGNOFF/// CHECKED THE HISTORY AND FOUND THE MED SEAL HAD BEEN REPLACED. INSPECTED SDR DXTA2023061688810Unknown · defectiveEMERGENCY LIGHTING: EMERGENCY LIGHTING DOES NOT COME IN WHEN AIRCRAFT IS SHUTDOWN WITH BATTERIES CONNECTED AND EMER SWITCH IN ARMED OR ON.//CORRECTIVE ACTION//REMOVED AND REPLACED ALL EMEREGENCY LIGHT POWER SUPPLY'S IAW WITH CL-650 AMM 33-51-01 AND CL-650 SMM SDR DXTA2023060187530Unknown · unknownLOUD AIR NOISE COMING FROM MAIN DOOR DURING FLT. PRESSURIZED ACFT & DUPLICATED LOUD AIR NOISE. FOUND PASSENGER DOORS TOP STEPS BONDING WIRE CAUGHT BETWEEN DOOR & AIRFRAME. DISCOVERED CAUSE OF BONDING WIRE BEING LOOSE TO BE THAT PAX DOORS TOP STEPS MOUNTING BASDR DXTA2021092249190Light · defectiveEMERGENCY LIGHTING: THE FORWARD EMERGENCY ISLE LIGHT IS INOP. // SIGN OFF // POWERED AIRCRAFT AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW CL650 MM CH.33-51-00 NOTING ALL LIGHTS OPERATIONAL EXCEPT THE FORWARD FLOOR PATH IDENTIFIER ON THE CREDENZASDR DXTA2021070744800Pdu · defectiveFLAP: FLAP MOTOR CIRCUIT BREAKER FOUND TO BE POPPED INFLIGHT. NOT SURE WHEN IT OCCURED NO CAS INDICATION ACCOMPANIED THE TRIPPED C/B. REMOVED FLAP PDU ASSY. NEED OK TO INSTALL FLAP PDU INSTALLED FLAP PDU ASSY IAW CL650 AMM 27-52-01 INSP).RIGGING AND OPERATION
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.