- Owner type
- Co-owned, fractional ownership
- Serial number
- 20575
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 23, 2015
- Certificate issued
- December 5, 2025
- Expires
- December 31, 2032
- Mode S code
- AAA0D1
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 N784QSMatched 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 N784QSMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025061603865Uplock · out of rigMLG: UPON DEPARTURE WE GOT AN AMBER "GEAR DISAGREE", AND CYAN "PROX SYS FAULT" CAS MESSAGE. RAN THROUGH THE CHECKLIST AND THE CAS MESSAGE DISAPPEARED. CONTINUED FLIGHT WITH GEAR DOWN AND DIVERTED TO KSYR. CORRECTIVE ACTION: FOUND PX05 LEFT MAIN LANDING GEAR USDR DXTA2024092300587Engine · warning messageIN CLIMB DETENT IN A CLIMB APPROX 27000 FEET R ENGINE EXCEEDANCE CAS ILLUMINATED. WE DID NOT NOTICE A RED ENGINE INSTRUMENT BEFORE WE REDUCED POWER. CONTINUED CLIMB AT A REDUCED POWER SETTING, AND WHILE FNISHING CHECKLIST, N2 GRADUALLY CLIMBED TO 98.1 AND R ENSDR DXTA2024062112114Static Inverter · defectiveBAGGAGE COMPARTMENT ODOR: A NOTICEABLE ELECTRICAL WIRE BURN ODOR IN BAGGAGE/LAV AREA. REMOVED STATIC INVERTER P/N SSC 200 S/N 413 INSTALL STATIC INVERTER P/N SSC 200 S/N 743 IAW BORBARDIER AMM CH. 24-26-01 NEED TO CHECK OPS 06/24/2024 HM JH. RECEIVED AND INSTSDR DXTA2023041083890Fcu · defectiveFLAPS FAIL AMBER CAS: FLAPS FAIL IN FLIGHT. EXECUTED NO FLAP LANDING. VERIFIED SQUAWK. SENT MDC AND FCU NVM DOWNLOADS FOR REVIEW. RESET FLAPS AND STILL GOT FLAPS FAIL AMBER CAS. GAINED ACCESS TO FLAP CONTROL UNIT (FCU} - REMOVED EXISTING UNIT, AND REPLACED SDR DXTA2021102150670Unknown · smokeAFTER TAKEOFF ON ENGINE BLEEDS, SMOKE STARTED COMING OUT OF THE SIDE AIR VENTS IN THE COCKPIT. SMOKE WAS WHITE & HAD AN OILY ODOR. NO ABNORMAL INDICATIONS OR CASS MESSAGES. ONCE AIR SOURCE KNOB ON AIR CONDITIONING/ BLEED PANEL WAS TURNED TO OFF, THE SMOKE SDR DXTA2020082424015Pump · defectiveCUAN "R DC HYD FAIL" CAS MESSAGE DURING THE ENTIRE APPROACH PHASE. CHECKED R DC PUMP ON GROUND, GOT RED HYD PRES LOW MESSAGE. 0 PSI IN RIGHT LINE WITH AMBER HYDRAULIC LINES ON HYDRAULIC SYSTEM PAGE. NO B-3 CODE IN SYSTEM. PER FSR, POWERED UP AIRCRAFT APU ASDR DXTA2019071502608Pump · failed1 HYDRAULIC PUMP - CYAN L HYD ENGINE PUMP FAIL ILLUMINATED AT FL410. A SHORT PERIOD LATER A CYAN L ENGINE FAULT ILLUMINTED. INITIAL HYDRAULIC SYSTEM SYNOPTICS INDIDATED THAT THE RESERVIOR CONTENTS WERE NORMAL. APPROXIMATELY 12-15 MINUTES LATER THE RESERVIOR COSDR DXTAT2PL6D005FW5QPump · leakingAT FL430, THE MASTER WARNING CHIMED AND A RED CAS RIGHT ENGINE OIL PRESSURE LOW DISPLAYED ON THE EICAS. THE RIGHT ENGINE OIL PRESSURE DIGITS WERE RED READING 25 AND DECREASING. PER THE CHECKLIST WE SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. AFTER LANDING,
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