- Owner type
- Co-owned, fractional ownership
- Serial number
- 9648
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 1, 2015
- Certificate issued
- November 5, 2025
- Expires
- November 30, 2032
- Mode S code
- A0C1D7
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 N148QSMatched 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 N148QSMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026082409378Engine · unknownAT ABOUT 200-300 FT AGL ON TAKEOFF, TOWER INFORMED SAW SMOKE COMING FROM ONE ENG. DEPARTED RUNWAY 12 AT KTUS WHICH PUT RT ENG ON TOWER SIDE, BUT TOWER COULD NOT TELL WHICH ENG SMOKE COMING FROM. THEY ALSO DID NOT DESCRIBE THE SMOKE IN ANY MANNER. RETURNED TSDR DXTA2025101305237Probe · defectiveDURING FLT, AMBER FUEL IMBALANCE CAS MESSAGE CAME ON IMMEDIATELY, RT SIDE INCREASE BY 2900 LBS. TOTAL FUEL ALSO INCREASED BY 2900 LBS. FOLLOWED QRH FUEL IMBALANCE. FUEL IMBALANCE BEGAN TO CORRECT. IMBALANCE CONINTUED TO CORRECT & STOPPED. TOTAL FUEL BEGAN SDR DXTA2025081504613Fuel Sys · out of balanceTHE FUEL QUANTITY INDICATED ON RIGHT GAUGE WAS SHOWING A COUPLE THOUSAND POUNDS MORE THAN IT ACTUALLY HAD. THE RESULT WAS INACCURATE FUEL TRANSFERRING LEADING TO FUEL IMBALANCE. THIS HAPPENED FOR 2 HOURS AND THEN RETURNED BACK TO NORMAL INDICATIONS. TROUBLESDR DXTA2024111201103Unknown · odorODORS IN COCKPIT / CABIN: ACRID SMELL IN LAV AND AFT BAGGAGE COMPARTMENT SMELLS LIKE SOME THING ELECTRICAL BURNING , PAX DID NOT SMOKE IN AIRCRAFT CORRECTIVE ACTION; UNABLE TO DUPLICATE. PERFORMED ENGINE IDLE RUNS. AND APU ON FOR 2 HOURS WITH ACM ON COLD AND HSDR DXTA2024110400999Sensor · defectiveL FADEC FAIL AMBER CAS: L FADEC FAIL AMBER CAS ILLUMINATED AT APPROXIMATE ALTITUDE MID 30,000S APPROXIMATE MACH .80. CONDITIONS WERE VMC AND ANTI ICE SELECTORS WERE IN AUTO WITH THE ANTI ICE NOT ACTIVE. THE EICAS MESSAGE ILLUMINATED AT 16:38 Z. CREW INITIASDR DXTA2024080700122Motor · noneEVALUATE MAIN CABIN DOOR MOTOR. MOTOR DOESN'T SEEM TO PROBIDE ENOUGH TENSION ON THE DOOR TO BE ABLE TO MOVE THE LOCK HANDLE INTO THE LOCKED POSITION. INSPECTED MAIN CABIN DOOR, PERFORMED MULTIPLES CYCLES FROM OUTSIDE IN MANUAL AND AUTO. FROM INSIDE PERFORMEDSDR DXTA2023052587020Unknown · unknownCARGO / BAGGAGE DOORS (LADDERS): DURING TAXI OUT FOR TAKE-OFF, AMBER CARGO DOOR CAS MESSAGE ILLUMINATED AND EXTINGUISHED APPROXIMATELY THREE TIMES. THE AMBER CARGO DOOR CAS MESSAGE THEN ILLUMINATED AND REMAINED ILLUMINATED THROUGH SHUTDOWN.SDR DXTA2022011255080Smoke Detector · defectiveSMOKE AVIONICS BAY RED CAS: ON CLIMBOUT OF DAL PASSING THROUGH FL210 WE RECEIVED A RED ' SMOKE AVIONICS BAY' CAS MESSAGE. WE DECLARED AN EMERGENCY , ACCOMPLISHED ALL CHECKLISTS AND RETURNED BACK TO DAL. // SIGNOFF// INSTALLED CUSTOMER SUPPLIED NEW SMOKE DETECTSDR DXTA2021092749430None · damagedMAIN DOOR MOTOR: MAIN ENTRY DOOR MOTOR RUNNING CONTINUOUSLY UNCOMANDED AFTER POWER UP AND WITH APU SHUTDOWN *** CORRECTIVE ACTION *** RDE1 FOUND TO HAVE WATER DAMAGE, REDE REPLACED IAW AMM 44-10-40-000/400-801 AND TESTED IAW SMM 44-10-50-710-801 WITH NIL FINDISDR DXTA2021090348090Relay · defectiveMAIN DOOR MOTOR SWITCH: MAIN CABIN DOOR INTERIOR SWITCH IS AMBER IN COLOR AND WILL NOT ACTIVATE DOOR. CMS DIAGNOSTICS CURRENT FAULTS SHOWS RELAY DRIVE EQUIPMENT RDE 1 INTERNAL FAILURE FAILED/WIRING // SIGNOFF // GAINED ACCESS TO RDE #1 AND REMOVED. UNIT HAS SISDR DXTA2018121091782Valve · leakingAVIONICS BAY SMOKE RED EICAS ON IMMEDIATELY AFTER TAKEOFF. NO EVIDENCE OF ANY SMOKE OR ELECTRICAL FIRE IN AVIONICS BAY, PERFORMED DETAILED GVI AND
NOTED SOME RESIDUAL WATER IN AVIONICS BAY FLOORBOARD. LOOKED FOR SOURCE OF WATER LEAK, UNABLE TO LOCATE SOURCESDR DXTA2018120321750Light · shortedCOCKPIT MAP LIGHT DID NOT ILLUMINATE - LEFT MAP LIGHT LOOSE AND INOP WHEN ADJUSTED SMOKE APPEARED FROM MOUNTING STEM AND ARCHING SOUND AUDIBLE CYAN CB TRIP AND EMS MAP LIGHTS CB TRIP IS INDICATED. REMOVED DEFECTIVE PILOT MAP LIGHT
ASSY P/N# 2LA456026-00 S/N SDR DXTA201808231283Controller · malfunctionedDURING ENGINE START AT DESTINATION, HAD BOTH CYAN LEFT AND RIGHT BLEED FAULT CAS MESSAGES AFTER ENGINE START. VERIFIED ON GO, NO GO, OK. AFTER TAKEOFF AND AFTER WING ANTI-ICE SWITCH WAS PLACED ON THE TRIM AIR FAULT CAS MESSAGE AND WING ANTI-ICE CAS MESSAG
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