- Owner type
- Co-owned, fractional ownership
- Serial number
- 9555
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 24, 2014
- Certificate issued
- July 31, 2025
- Expires
- July 31, 2032
- Mode S code
- A014FF
Bombardier BD-700-1A11TCDS T00003NYAirframe · Bombardier BD-700-1A11TCDS E00057ENEngine · Rolls-Royce Deutschland BR700-710A220
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 71
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1999 | 1 |
|---|---|
| 2001 | 2 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 4 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 6 |
| 2017 | 4 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 5 |
| 2022 | 4 |
| 2023 | 10 |
| 2024 | 4 |
| 2025 | 7 |
| 2026 | 6 |
Airframe · Bombardier BD-700-1A11
AD 2026-15-09Landing GearAD 2026-11-07Equipment/furnishingsAD 2026-13-02NavigationInformation bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N104QSMatched 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 BD-700-1A11 aircraft
FAA incident reports
No FAA accident or incident reports matched to N104QSMatched 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 BD-700-1A11 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 3J7R2024005220001Battery Pack · no testDURING MAINTENANCE CHECK FOUND MAIN ENTRY EXIT LIGHTED SIGN INOPERATIVE.SDR DXTA2023111010014Unknown · unknownMAIN DOOR: IN FLIGHT, PASSENGER DOOR AMBER MESSAGE ILLUMINATED ON AND OFF FOR ENTIRE FLIGHT. WE RAN THE QRH. NO PRESSURE SPIKES NOTED. FOUND INTERMITTENT CONNECTION BETWEEN PINS J AND K ON CONNECTOR P452. FOUND LOOSE SPLICE WIRE DAH0732W-22. REPAIRED SPLICE ISDR DXTA2023092696510Unknown · unknownMAIN DOOR: WHILE PREPARING FOR ENGINE START WITH DOOR CLOSED .. PASSENGER DOOR CAS MESSAGE CAME ON 4 DIFFERENT TIMES. WE OPENED AND CLOSED DOOR BUT MESSAGE STILL CAME BACK. REMOVED AND REPLACED THE FORWARD AND AFT G LOCK AND THE OUTER HANDLE PROXIMITY SWITCH SDR DXTA2023091995850Proximity Switch · faultedPASSENGER DOOR AMBER CAS: DESCENDING THRU FL 180, PASSENGER DOOR AMBER CAS ILLUMINATED SEVERAL DIFFERENT TIMES, THEN REMAINED ON CONTINUOUSLY UNTIL LANDING AND PARKED. DOOR CLOSED NORMALLY AND PRESSURIZATION APPEARED NORMAL. FOUND FAULT CODE 3232117EL SEVERALSDR DXTA2023071490880Actuator · defectiveMAIN ENTRY DOOR WILL NOT CLOSE WITH EITHER INSIDE OR OUTSIDE DOOR SWITCHES. WHEN EITHER SWITCH IS DEPRESSED, AFTER APPROX. :05 SECONDS, THE LOWER HINGED STEP FOLDS EXTREMELY SLOWLY, BUT DOOR MOTOR IS NOT RUNNING. REMOVED PASSENGER DOOR ACTUATOR DUE TO BURNED SDR DXTA2022081668130Proximity Sensor · out of rigMAIN DOOR PRIMARY SEAL: AFTER TAKE OFF WE GOT A PASSENGER DOOR CAS. THE CAS FLASHED ON AND OFF SEVERAL TIMES AND THE PLANE WOULD NOT PRESSURIZE AT ALL.//CORRECTIVE ACTION// RE-RIGGED MAIN CABIN DOOR HANDLE PROX SWITCH, REPLACED FOOTBALL SPLICE DUE TO BROKEN WISDR DXTA2022080467300None · noneMAIN DOOR: "PASSENGER DOOR" CAS MESSAGE CAME ON MULTIPLE TIMES IN FLIGHT, INCLUDING YELLOW DOOR SYMBOL ON SYNOPTIC PAGE. PRESSURE DIFFERENTIAL REMAINED NORMAL. PERFORMED GENERAL VISUAL INSPECTION OF MAIN CABIN DOOR, NO FAULTS NOTED. OPERATED DOOR THROUGH SEVSDR DXTA2022021256610Not Reported · not reportedMAIN DOOR: PASS DOOR AMBER CAS CAME ON 9 TIMES AND WENT OUT EACH TIME MX CODE 3231117EL///SIGN-OFF///FOUND LOWER SWITCH OUT OF RIG. RIGGING FOUND TO BE 0.056. TECHS RERIGGED TO 0.039 INCH SPECIFIED TOLERANCE RANGE 0.030-0.050 INCH. OPS CHECK GOOD. IAW GL-5SDR DXTA2021071945480Warning Message · false activationMAIN DOOR: AFTER ROTATION PASSENGER DOOR AMBER CAS MESSAGE ILLUMINATED. DOOR SCHEMATIC ALSO CONFIRMED DOOR UNLOCK CONDITION . CAS MESSAGE CYCLED ON AND OFF FOR ENTIRE 15 MINUTE FLIGHT. FLEW UP TO 5000 FT FOR TERRAIN CLEARANCE AND THE AIRCRAFT DID NOT PRESSDR DXTA2016012406170Seal · leakingCABIN FAILED TO PRESSURIZE IN FLIGHT. AIR COULD BE HEARD LEAKING PAST THE DOOR SEAL. COMPLIED WITH RIGGING CHECK WITH NO DEFECTS NOTED. IAW AMM 52-11-00 ALSO PERFORMED MULTIPLE OPERATIONAL TEST WITH NO DEFECTS NOTED. PERFORMED SATISFACTORY ACFT PRESSURIZATSDR DXTA2014110305920Wire · mismarkedRIGHT POWER OUTLET IN GALLEY, BELOW OVEN CONTROLS, SPARKED & BURNED ANY DEVICE THAT WAS PLUGGED INTO IT. REMOVED DEFECTIVE GALLEY OUTLET & INSTALLED A NEW OUTLET. BEFORE INSTALLATION NOTICED THAT THE WIRES DID NOT MATCH TO THE LABELS GOING TO THE OUTLET.
STCs that may be installed · 141
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 141 STCs