- Owner type
- Co-owned, fractional ownership
- Serial number
- 20651
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 11, 2016
- Certificate issued
- April 6, 2026
- Expires
- April 30, 2033
- Mode S code
- A9CC7A
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-2-1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 1 |
|---|---|
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 5 |
| 2018 | 4 |
| 2019 | 3 |
| 2020 | 3 |
| 2021 | 6 |
| 2022 | 5 |
| 2023 | 9 |
| 2024 | 8 |
| 2025 | 1 |
| 2026 | 3 |
Airframe · Bombardier BD-100-1A10
AD 2026-13-02NavigationAD 2026-02-06Flight controlsAD 2026-01-07Time Limits/Maintenance ChecksInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Bombardier BD-100-1A10
SAIB AIR-22-02R1Pitot/Static Anti-Ice SystemSAIB NM-18-32R1Electrical Power - Direct Current Power CenterNTSB investigations
No NTSB investigations matched to N730QSMatched 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-100-1A10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N730QSMatched 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-100-1A10 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025072104287Acm · smokeDURING CLIMB AT 1500 FEET AND AFTER SWIRCHING THE BLEEDS FROM APU TO ENGINES, WE SAW SMOKE COMING OUT OF ALL VENTS IN THE COCKPIT AND SMELLED WHAT WE BELIVE IS ENVIRENMENTAL SMOKE. WE DECLARED AN EMERGENCY AND LANDED ABIUT 10 MINUTES LATER. THE TEMPERATURE IN SDR DXTA2025012302073Brake · smokeLEFT MLG BRAKE: AFTER NORMAL LANDING AND TAXIING TO CUSTOMS RAMP, CUSTOMS AGENTS NOTICED SMOKE COMING FROM L MAINS. I LOOKED AND ALSO SAW THE SMOKE AS WELL AS FLUID DRIPPING FROM L OUTBOARD BRAKE. AS PRECAUTION, WE DECIDED TO GET TUGGED OVER TO RAMP ONLY TO SDR 2024FA0000826Skin · crackedON THE LOWER FUSELAGE SKIN AT FS 422 & 779 CORROSION WAS FOUND AROUND THE FASTENER HOLES WHERE THE LOWER FUSELAGE TO WING FAIRINGS ATTACH. AFTER REMOVING THE CORROSION AND THE EVALUATION DETERMINED THE SKIN IN THOSE AREAS WAS OUT OF LIMITS. ENGINEERING WAS REQSDR DXTA2024010210476Adc · faultedDURING CLIMB, THRU 18,000, AN EFIS MISCOMPARE CAS MESSAGE DISPLAYED FOLLOWED BY AN ALT MISCOMPARE BOX. COMPARING 3 SYSTEMS, DTEREMINED THE LT SIDE ADC AT FAULT. ALTITUDE & AIRSPEED WERE BOTH INCORRECT. STOPPED CLIMB & DESCENDED TO FL 200. HAD MANY CASCADINGSDR DXTA2023051986550Sensor · defectiveON DESCENT AT AROUND 6,000 FT & APPROXIMATELY 250 KTS FLAP FAIL EICAS ILLUMINATED. RAN FLAP FAIL QRC AND DIVERTED TO SWF FOR A LONGER RUNWAY. FLAP FAIL MESSAGE REMAINED ILLUMINATED THROUGH SHUTDOWN. DIAGNOSTIC DATA: POSITION SENSOR FAULT ID# B3-007120. POWERSDR DXTA2021090748270Door · bindingMAIN DOOR: THE MAIN CABIN DOOR IS VERY DIFFICULT TO CLOSE. YOU NEED TO REALLY PUSH ON IT TO GET IT CLOSED FROM THE EXTERIOR. WHEN CLOSING IT FROM INSIDE IT TAKES A GOOD BIT OF PULLING ON IT TO GET IT CLOSED. PERFORMED A FUNCTIONAL TEST OF THE MED WITH NO DEFESDR DXTA2021041240670Battery · inoperativeCABIN EMERG LIGHT: THE EMERGENCY LIGHTS UNDER SEAT 4R ARE ON WITH THE EMER LTS SWITCH IN THE ARM AND OFF. IN THE ON POSITION, ALL LIGHTS ARE ON, AS THEY SHOULD BE. PICTURE INCLUDED // SIGNOFF // VERIFIED DISCREPANCY. SWITCHED THE LIGHT FROM SEAT 4R WITH LIGHT
Reports on N730QS not matched to an aircraft · 10
They name N730QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2012031604922Altimeter · inoperativeAFTER DEPARTURE AT APPROX 3000" IN CLIMB, RED GEAR NOT DOWN CAS MESSAGE CAME ON ALONG WITH GEAR HORN. BOTH RADAR ALTIMITERS FLUCUATED WITH A RANGE OF RA ALTITUTDES MUTIPLE TIMES, EVENTUALLY THE LT RA SHOWED 0 FOR THE REMAINDER OF THE FLIGHT WHILE THE RIGHT RASDR DXTA2009090803774Actuator · malfunctionedA/P PITCH TRIM CAUTION LIGHT CAME ON WHILE CLIMBING THROUGH 10-12 THOUSAND FEET. UPON DISENGAGING THE AUTO PILOT, ACFT PITCHED UP SLIGHTLY DUE TO NOSE UP PITCH SETTING, PITCH TRIM ADJUSTED BACK DOWN WITH THE NORMAL TRIM SWITCH AND CAUTION LIGHT WENT OUT. UPSDR DXTA2009010403458Actuator · inoperativeGEAR FAILED TO RETRACT (CYCLED GEAR PER QRH STILL UNABLE TO RETRACT) (AMBER LT MAIN GEAR INDICATOR TURNED RED - SELECTED DOWN - GOT 3 GREEN IAW QRH). REMOVED AND REPLACED LT MLG ACTUATOR WITH A REPAIRED UNIT. ALL LK AND OPS CK ARE COMPLIED WITH NO OTHER DEFEC
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