- Owner type
- Co-owned, fractional ownership
- Serial number
- 60117
- Year built
- 2024
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 27, 2024
- Certificate issued
- April 17, 2024
- Expires
- April 30, 2031
- Mode S code
- A07690
Bombardier BD-700-1A11TCDS T00003NYAirframe · Bombardier BD-700-1A11TCDS E00057ENEngine · Rolls Deu BR700-710D521
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 60
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 2 |
|---|---|
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 5 |
| 2017 | 4 |
| 2018 | 4 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 3 |
| 2022 | 4 |
| 2023 | 9 |
| 2024 | 4 |
| 2025 | 6 |
| 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 N129QSMatched 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 N129QSMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026021606885Battery Pack · faultedAFT OVER WING EMERGENCY LIGHT IS INOP CORRECTIVE ACTION: AND REMOVED POWER SUPPLY DUE TO LIGHT BEING INOP. INSTALLED CUSTOMER SUPPLIED REPAIRED POWER SUPPLY IAW AMM 33-51-09, OPS CHECKED GOOD.SDR DXTA2025021702362Pump · faultedHYDRAULIC FLUID: SYSTEM 3 VOLUME LEAKED DOWN TO 0. REPLACED HYDRAULIC PUMPS. OPS CHECK AND LEAK CHECK GOOD. IAW GL5500 AMM 29-13-01.SDR DXTA2024070112215Brake Sys · failedON APPROACH AFTER SELECTING FLAPS 30 WE GOT AMBER BRAKE 50% DEGRADE ALONG WITH AMBER AUTO BRAKE FAIL MESSAGE. RAN ABNORMAL CHECKLIST . ON LANDING ROLL OUT THE MESSAGES WENT AWAY . PICTURE INCLUDED OF BRAKE TEMPS ARE HIGHER ON THE LEFT THEN ON THE RIGHT. I BARSDR DXTA2024070112214Brake Sys · failedAUTOBRAKE FAIL AMBER CAS: ON APPROACH AFTER SELECTING FLAPS 30 WE GOT AMBER AUTO BRAKE FAIL ALONG WITH AMBER BRAKE 50% DEGRADE. RAN ABNORMAL CHECKLIST . AT SOME POINT ON LANDING ROLL OUT THE MESSAGES WENT AWAY. BRAKE TEMPS ON THE LEFT SIDE ARE A LOT HIGHER TSDR DXTA2024052711864Proximity Switch · failedRIGHT EMER EXIT CAS ILLUMINATED IN FLIGHT AND REMAINED ON UNTIL ON THE GROUND. CABIN SYNOPTIC SHOWED EMER EXIT DOOR OPEN IN FLIGHT AS WELL. CHECKLIST COMPLIED WITH. ADJUSTED THE PROXITMITY SWITCH GAP OPS CHECKS GOOD.
Reports on N129QS not matched to an aircraft · 10
They name N129QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR BJ6A2009090812901Cover · dislodgedON 9/6/2009 DURING THE TAKEOFF ROLL, CREW NOTICED THE MASTER WARNING LIGHT ILLUMINATED. CREW ABORTED THE TAKEOFF BELOW 80 KTS. ONCE CLEAR OF THE RUNWAY THE CREW DETERMINED THE SOURCE OF THE WARNING WAS THE OFFICE AREA SMOKE DETECTOR. FURTHER INVESTIGATION RSDR BJ6A200712901Charger · failedDURING GROUND OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM, SEVERAL EMERGENCY LIGHTS AT THE AFT LAVATORY AREA AND L2 DOOR FAILED TO ILLUMINATE. REPLACED EMERGENCY BATTERY CHARGER TO RESTORE NORMAL OPERATION.SDR BJ6A200612903Floorbeam · corrodedGALLEY FLOOR STRUCTURE FOUND CORRODED WHEN GALLEY WAS REMOVED FOR OTHER MAINTENANCE. REPAIRED FLOORBEAM IAW DRAWING 4182527-01 AND SRM 51-10-51. NEW MOISTURE PROTECTIVE BARRIER APPLIED UNDERNEATH FLOORING MATERIAL AND THE FLOORBOARDS. THE CORROSION APPEARS TO
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