- Owner type
- Co-owned, fractional ownership
- Serial number
- 20695
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 12, 2017
- Certificate issued
- July 29, 2021
- Expires
- July 31, 2028
- Mode S code
- A9FF1E
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-2-1A
From the FAA registry file of October 27, 2026.
On this page
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N743QSMatched 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
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 CenterService difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026011506537Hand Rail · damagedMAIN PASSENGER DOOR RAILING STUCK IN THE UP POSITION. DOOR CAN'T CLOSE. REMOVED DAMAGED HANDRAIL (P/N 1005210201-001 S/N E12) AND HANDRAIL FITTING. INSTALLED NEW CUSTOMER SUPPLIED HANDRAIL (P/N 1005210201-001 S/N T2PL6D00DKNBV) AND HANDRAIL FITTING. WORK PERSDR DXTA2025101405282Elec Connector · incorrectAFTER LANDING AND SHUTTING DOWN REGARDLESS OF THE EMERGENCY LIGHT SWITCH POSITION THE RED EMERGENCY LIGHT UNDER SEAT 4R STAYS ON. UPON INITIAL POWER UP WE WERE UNABLE TO DUPLICATE FAULT. DURING OP CHECK OF EMERGENCY LIGHTS FOUND SEAT 4R TO FAIL TEST. AFTER FSDR 2025FA0000679Support Angle · corrodedDURING A FUSELAGE EXTERIOR INSPECTION FOUND CORROSION AND THE SUPPORT ANGLE BELOW THE AFT ENTRY DOOR THRESHOLD AROUND THE FASTENER NUTPLATES.SDR DXTA2023102698880Unknown · unknownMAIN DOOR: MAIN DOOR OPENED NORMALLY BUT ON 3RD ENTRY THE DOOR DROPPED SEVERAL INCHES. SOMETHING GAVE WAY AND THE DOOR WILL NOT TAKE WEIGHT WITHOUT MAKING CONTACT WITH THE FUSELAGE. THE DOOR WILL NOT CLOSE PROPERLY. MAIN DOOR BEARINGS AND INTERNAL LOCKING POISDR DXTA2022080167110None · noneMAIN HYDRAULICS: UPON INTIAL TAXI OUT, AMBER "OUTBD BRAKES FAIL" ILLUMINATED. RAN APPROPRIATE CHECKLIST. NO CHANGE. B3-007113 // SIGNOFF// PULLED AND RESET CB: RCBP-C15 AND PERFORMED THE HARDWARE MONITOR TEST, PERFORMED THE BCU EPROM AND THE BCV RESISTANCE TESSDR DXTA2022052362360Display · failedIFIS: PILOTS SIDE PFD FAILED, BLACK SCREEN. COPILOTS PFD HAD RAW DATA ONLY. AMBER PDF X TALK FAIL ILLUMINATED. AMBER EFIS MISCOMPARE ILLUMINATED AUTO PILOT AND FLIGHT DIRECTOR FAILED. FOLLOWED CHECKLIST. // SIGNOFF// ACCESSED AIRCRAFT AND APPLIED EXTERNAL POWSDR DXTA2020080103923Panel · brokenENROUTE, A PASSENGER GOT STUCK IN THE LAV AND COULD NOT RELEASE THE LOCK. WE TRIED MULTIPLE OPTIONS, CALLED MAINTENANCE, AND TRIED MORE OPTIONS. WITH NO AVAIL TO OPEN DOOR, WE WERE INSTRUCTED BY MANAGEMENT TO BREAK DOOR TO GET THE PASSENGER FREE. WE KICKED SDR DXTA2019070202560Ecu · malfunctionedPRI STAB TRIM FAIL AMBER CAS ILLUMINATED - WITH GEAR DOWN SELECTED FLAPS 10 WHILE DESCENDING. GOT AP HOLDING NOSE UP CAS AND AP STAB TRIM FAIL CAS MESSAGES. RAN QRH FOR AP STAB TRIM FAIL AND THEN GOT PRI STAB TRIM FAIL CAS MESSAGE. RAN QRH GOT SECONDARY TRIM BSDR DXTA2019051302389Radio Altimeter · defectiveGEAR RED CAS ILLUMINATED - AFTER TAKE OFF DURING CLIMB RED CAS MESSAGE"GEAR". DISAPEARED AFTER 1 SECOND. (INCLUDED CAS MESSAGE "SPOILER FAULT") SPEED 250 AT 6000 FT CLIMBING. CORRECTIVE ACTION, DOWNLOADED FAULT HISTORY AND SPOILER ECU FAILT HISTORY. SENT FILES
Reports on N743QS not matched to an aircraft · 8
They name N743QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015111306121Unknown · smokeUPON TAKEOFF, THE CABIN & COCKPIT FILLED WITH SMOKE. AFTER COMPLETING SEVERAL VISUAL INSP & CLEANING OF RESIDUAL OIL, RAN APU BLEED AT HIGH FLOW ON MAX HEAT FOR 15 MINS TO START DUCT BURN OUT PROCEDURE. STARTED ACFT ENGS, RAN LT ENG AT HIGH POWER WITH ECS SESDR DXTA2014090805875Brake Sys · contaminatedDURING ACFT MOVEMENT WITH BRAKES INITIALLY APPLIED A GROANING SOUND CAN BE HEARD UNDER COCKPIT FLOOR. WITH PARK BRAKE SET A THUMPING SOUND CAN BE HEARD BELOW PEDESTAL. EXCESSIVE BRAKE PRESS SEEMS TO BE REQUIRED TO RECEIVE NORMAL BRAKING ACTION AT TAXI SPEED.SDR DXTA2014041405728Uplock Switch · inoperativeRIGHT MAIN GEAR WOULD NOT INDICATE UP. COMPLIED WITH QRH PROCEDURES. R & R RT MLG NR 2 UPLOCK SWITCH IN THE AFT POSITION IAW AMM 32-10-11. PERFORMED EXTENSION & RETRACTION FUNCTIONAL TESTS IAW AMM 32-30-00. OPS CHECKED GOOD.
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