- Owner type
- Corporation
- Serial number
- 9557
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 11, 2014
- Certificate issued
- June 30, 2026
- Expires
- June 30, 2033
- Mode S code
- A0FE42
Bombardier BD-700-1A10TCDS T00003NYAirframe · Bombardier BD-700-1A10TCDS E00057ENEngine · Rolls-Royce Deutschland BR700-710A220
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 75
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 | 3 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 4 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 2 |
| 2016 | 6 |
| 2017 | 4 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 7 |
| 2022 | 4 |
| 2023 | 10 |
| 2024 | 4 |
| 2025 | 8 |
| 2026 | 6 |
Airframe · Bombardier BD-700-1A10
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 N163QSMatched 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-700-1A10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N163QSMatched 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-700-1A10 aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026010906458Distribution Box · faultyIN FLIGHT WE GOT A CYAN R PROBE MON FAIL MESSAGE, WHICH THEN TRIGGERED THREE AMBER CAS MESSAGES: R AOA HEAT FAIL, PITOT 2 HT FAIL AND STBY PITOT HT FAIL. THIS ALL BEGAN WHEN THE HBMU 2 CIRCUIT BREAKER TRIPPED ON THE EMS-CDU. T/S SYSTEM, REMOVED SUSPECTED HBSDR 3J7R2025120500001Power Supply · inoperativeEXIT SIGN ON FWD BULKHEAD IN THE CABIN ABOVE SEAT 1 INOPERATIVE.SDR DXTA2025102005329Actuator · failedWHILE CLOSING MED DOOR, SOMETHING CAME LOOSE & ENTIRE DOOR CAME SLAMMING DOWN. MX CORRECTED THE PAX DOOR DISCREPANCY BY REMOVING UNSERVICEABLE DOOR ACTUATOR & REPLACING IT WITH A REPAIRED SERVICEABLE UNIT IAW AMM 52-11-25-400-801, FOLLOWED BY FULL RIGGING OF SDR DXTA2025050203304Wire Harness · faultedAIR DATA COMPUTER: AFTER TAKEOFF WINDSHEAR ON THE PFD DISPLAYED FOLLOWED BY AUTO THROTTLES OFF AND THE AUTO PILOT WOULD NOT RE-ENGAGE. BOTH PFDS HAD MULTI FAILURES AND THEN BEGAN FLASHING AND SWITCHING BETWEEN SVS ON AND OFF. AFTER TURNING OFF SVS SOME OF TSDR DXTA2025012702075Door · damagedAFTER GEAR RETRACTION, FOUND NLG AFT DOOR DAMAGED. CORRECTIVE ACTION: REPLACED DOOR. OPS CHECK GOOD. IAW BOMBARDIER GL6000 AMM 32-22-05-000-801.SDR DXTA2023102798930Control Handle · faultedON GEAR RETRACTION GOT MLG UP BUT NLG DOOR DID NOT CLOSE, HEAVY VIBRATION & HAD CAS MSG MLG SYS FAIL & GEAR DISAGREE. CHECKED ALL SOLENOIDS, VALVES, AND WIRE, NO DEFECTS. R & R MLG CONTROL LEVER. PERFORMED OPS CHECKS AND OPS-CHECKS GOOD. WORK PERFORMED IRW SDR DXTA2023072891830Unknown · unknownGEAR DISAGREE AMBER CAS: NOSE GEAR RETRACTED, MAIN GEARSREMAINED DOWN AND GREEN UPON GEAR UP SELECTION. COMPLETED GEAR DISAGREE CHECKLIST, ALL CAS MESSAGES CLEARED WITH GREEN DOWN AND LOCKED INDICATIONS. REMOVED #2 MLG CONTROL VALVE. INSTALLED A NEW MLG CONSDR DXTA2023060587760Unknown · unknownMAIN DOOR: WHILE PREPPING FOR DEPARTURE. CREW NOTED CYAN CAS MSG: CB TRIPPED AND AMBER MSG: PASSENGER DOOR. CREW ALSO NOTED THAT USING THE EMS CIRCUIT BREAKER STATUS FUNCTION ON THE EMS PANEL: PAX DOOR MOTOR...AV BATT...DCPC...OUT. THE PASSENGER DOOR WILL NOTSDR DXTA2023050585370Actuator · defectiveNLG LANDING GEAR RETRACTION: UPON DEPARTURE, NOSE LANDING GEAR DID NOT RETRACT. APPROPRIATE CHECKLIST APPLIES AND GEAR EXTENTION WAS NORMAL. // SIGNOFF// GAINED ACCESS TO AIRCRAFT AND INTEROGATED OMS. DOWNLOADED LRU NVM AND ALL FAULTS. SENT TO BOMBARDIER --FORSDR DXTA2022120275300Selector Valve · defectiveGEAR DISAGREE CAS MESSAGE¿.AFTER RETRACTING THE GEAR WE RECEIVED 5 AMBER CAS MESSAGES AND 1 CYAN CAS MESSAGE. AMBER GEAR SYS FAIL, L MAIN GEAR DOOR, GEAR DISAGREE, R MAIN GEAR DOOR, NOSE DOOR FOLLOWED BY CYAN BRAKE FAULT CAS MESSAGE. ON THE SYNOPTIC PAGE WE HA
STCs that may be installed · 432
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 432 STCs