- Owner type
- Co-owned, fractional ownership
- Serial number
- 20562
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 29, 2015
- Certificate issued
- March 30, 2026
- Expires
- March 31, 2033
- Mode S code
- AA8477
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 N777QSMatched 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 N777QSMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025102005325Control Unit · defectiveON APPROACH SELECTED FLAPS 10. FLAPS TRACKED ONLY TO 2 DEGREES AND FLAP FAULT AMBER CAS APPEARED. COMPLIED WITH QRH SELECTED FLAPS BACK TO ZERO AND FLAPS FAIL AMBER CAS APPEARED. COMPLIED WITH QRH FOR ZERO FLAP LANDING. LANDED UNEVENTFULLY. B3 CODE #006786 FPSDR DXTA2025072504322Power Unit · faultedDURING APPROACH, FLAPS 10 WERE SELECTED & THE FLAPS MOVED UNTIL IT INDICATED 2 DEGREES & MOVEMENT STOPPED FOLLOWED BY AMBER CAUTION EICAS MESSAGE FLAPS FAULT & APPROXIMATELY 10 SECONDS LATER, AMBER EICAS MESSAGE FLAPS NORM PRESS LOW ALSO DISPLAYED. QRH GUIDEDSDR DXTA2025072204291Adc · defectiveIN LEVEL FLIGHT AT 6000 FT GEAR & FLAPS UP SPEED 250 KTS. WE GOT AN AMBER ALT BOX MESSAGE ON BOTH PFD'S AND AN EFIS MISCOMPARE ICAS MESSAGE. LEFT ALT (6000) RIGHT ALT (5850) STBY ALT (5800) RAN QRH AVNC 02-5 EFIS MISCOMPARE B3 CODE TO FOLLOW B3-007890 NO ADC-2SDR DXTA2024121901552Transducer · damagedSHORTLY AFTER A SMOOTH TOUCH DOWN (LESS THAN 10 KNOT CROSSWIND) AND SPOILERS DEPLOYED CALL OUT BY FO, THE FO ALERTED ME THAT NWS FAIL AMBER CAS WAS DISPLAYED ON EICAS. THERE WAS NO STEERING IN PEDALS NOR TILLER. USED DIFFERENTIAL BRAKING FOR STEERING. B3 CODESDR DXTA2024042511598Apu · leakingCABIN/COCKPIT HAS STRONG ACRID STENCH, SUSPECT ATOMIZED TURBINE OIL FROM AIR CYCLE MACHINE PASSED THE LABYRINTH SEAL. REMOVED APU P/N 3800774-1, S/N P-609 DUE TO SMOKE IN THE COCKPIT. INSTALLED A REPAIRED APU. OPS CHECK GOOD. IAW BOMBARDIER CL350 MM CH 49-SDR DXTA2024031111152Wire Harness · disconnectedTHE WIRING HARNESS FOR THE OPERATION OF THE MAIN CABIN DOOR IS UNPLUGGED. IT APPEARS THE VENEER HAS SEPARATED FROM THE FRAME OF THE INTERIOR, DISCONNECTING THE CABIN DOOR. THE INTERIOR LIGHTS ON THAT SWITCH ARE ALSO INOP. MAINTENANCE WAS ON THE AIRCRAFT ALLSDR DXTA2022082969010None · defectiveLAV EMERG LIGHT: THE RIGHT READING/EMERGENCY LIGHT ABOVE THE LAV DOES NOT ILLUMINATE WITH EITHER READING BUTTON, OR WITH EMERGENCY LIGHTS ACTIVATED. THE LIGHT IN QUESTION IS THE VERY AFT ROUND LIGHT ABOVE THE SEATED LAV. // SIGNOFF// GAINED ACCESS. REMOVED ANDSDR DXTA2016123006354Apu · odorON TAKEOFF THERE IS A STRONG DIRTY SOCK ODOR WHICH SEEMS TO DISSIPATE IN FLIGHT. THE APU IS OPERATING ON TAKEOFF UNTIL ABOUT 1000 AGL. ON ARRIVAL MAINTENANCE SAID THEY CAN STILL SMELL ODOR. REPLACED APU WITH AN INSPECTED UNIT AND PERFORMED SATISFACTORY OPESDR DXTA2016022906191Microwave Oven · failedWHILE AT 40000 FEET, TURNED MICROWAVE SWITCH ON FROM COCKPIT. FIRST OFFICER THEN WENT BACK TO GALLEY & SMELLED BURNING ELECTRICAL ODOR. ALSO NOTED THAT THE MICROWAVE DID NOT TURN ON EVEN THOUGH COCKPIT MICROWAVE SWITCH WAS ON. IT MAY HAVE COME FROM CB PANEL
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