- Owner type
- Co-owned, fractional ownership
- Serial number
- 20526
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 19, 2014
- Certificate issued
- March 23, 2026
- Expires
- March 31, 2033
- Mode S code
- AA5941
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 N766QSMatched 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 N766QSMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026081009150Wire Harness · damagedON INITIAL TAKEOFF LANDING GEAR HANDLE WAS RAISED AND RECEIVED GEAR DISAGREE CAS MESSAGE ALONG WITH PROX SYS FAULT MESSAGE. B3 CODE 007504. TOWER CONFIRMED ALL GEAR WERE IN THE UP POSITION WITH THE GEAR HANDLE UP. GEAR INDICATIONS SHOWED RIGHT MAIN AND NOSE UPSDR DXTA2026071708843Potentiometer · out of adjustSECOND WRITE UP. DURING LANDING ROLLOUT, THE NOSE WHEEL STEERING FAIL CASS MESSAGE APPEARED. UNABLE TO CONTROL NOSE WHEEL, STEERING WITH PEDALS OR TILLER. TECHS ARRVIED TO ACFT AND WERE UNABLE TO DUPLICATE THE FAULT, TECHS ATTEMPTED TO PERFORM THE NWS NVM DOWNSDR DXTA2026062408526Warning Message · illuminatedAFTER TAKEOFF AND SELECTING GEAR UP THE AMBER GEAR DISAGREE AND CYAN PROX SYS FAULT DISPLAYED ALONG WITH LT GEAR SHOWING EXTENDED WITH THE GEAR HANDLE IN THE UP POSITION. COMPLIED WITH CHECKLIST AND DIVERTED TO KIAD WITH NO FURTHER ISSUES. INTERROGATED THESDR DXTA2024072212409Engine · surgesDURING TAKEOFF, IMMEDIATELY AFTER ACFT BECAME AIRBORNE, HEARD 3-4 LOUD BANGS FROM WHAT SOUNDED LIKE THE LT ENG. BELIEVE IT WAS POSSIBLY A COMPRESSOR STALL. RIGHT ENG UNEXPECTED SURGE. BELIEVE THE RT ENG SURGE WAS DUE TO THE LT ENG COMPRESSOR STALL. C/W ENSDR DXTA2024040211378Unknown · odorTHERE IS A STRONG SMELL OF FUEL IN THE COCKPIT DURING TAKEOFF ROLL. UNABLE TO ISOLATE WHERE ITS COMING FROM BUT ITS VERY APPARENT DURING TAKEOFF AND CLIMB OUT. INSPECTED AND WIPED DOWN ENGINES AND COWLINGS OPERATED ENGINES AT HIGH POWER SETTINS FOR 7 MINUTESDR DXTA2024022911032Cable · failedCLOSING CABIN DOOR. DOOR ELEVATED ABOUT A FOOT OFF GROUND WHEN I FORGOT SOMETHING. RELEASED BLACK DOOR CLOSE BUTTON TO ALLOW DOOR TO FALL OPEN. WHEN DOOR REACHED FULL OPEN, HEARD A SNAP. PULLEY AT TOP OF STAIRS FOUND BROKEN & CABLE FRAYED & NOT IN PULLEY. NO SDR DXTA2023083194290Connector · disconnectedINTERIOR CABIN EMERGENCY LIGHTS ABOVE SEATS 2L AND 3R DON NOT ILLUMINATE WITH EMER LIGHT SWITCH PLACED TO ON FOR PREFLIGHT. GAINED ACCESS TO POWER SUPPLIES IN LOWER SIDEWALL AND BEHIND GALLEY AND SWAPPED POWER SUPPLIES PN 2013-1A SN 120510 AND PN 2013-1A SN 1SDR DXTA2023081092680Unknown · unknownUPPER EXIT SIGN AT THE TOP OF THE MED STAIRS DOES NOT ILLUMINATE WHEN SELECTED ON. UPON INVESTIGATING MAIN ENTRY DOOR UPPER EXIT SIGN LIGHT, WE DISCOVERED A LOOSE CONNECTION ON THE CONNCETORS ON THE BACK OF THE EXIT SIGN LIGHT. RECONNECTED THE CONNECTORS TO SSDR DXTA2023051085800Unknown · unknownL OUTBD BRAKE FAIL AMBER CAS: ON FINAL CAS MSG,.. LANDED NORMALLY,.. UPON PARKING HYD FLUID STEAMING FROM WHEEL WELL ONTO WHEELS AND PUDDLING ON GROUND B3-007115,.. L OB BRAKE PRESS PULSESDR DXTA2019092202871Engine · power lossLEFT ENGINE ENGINE COMPRESSOR STALL EVALUATE - ON TAKEOFF FROM TEB RUNWAY 24 WE EXPERIENCED TWO SUBSTANTIAL AIRFRAME SHUDDERS AFTER POWER REDUCTION AND DURING GEAR RETRACTION AT ABOUT 500' AGL 170KTS FLAPS 10. THERE WERE NO COCKPIT INDICATIONS OR WARNINGS. UPOSDR DXTA2018092701468Entertain Sys · malfunctionedADDED INFO: APPROACHING RWY 22R ON TAXIWAY N, CREW DETECTED AN UNUSUAL ODOR IN THE AIRCRAFT... POSSIBLY FM THE FLIGHT DECK VENTS OUTBOARD OF THE SEAT ARM RESTS. BOTH ENGINES & THE APU WERE RUNNING. THE ECS WAS ON THE APU. CREW & PAX OBSERVED LIGHT GRAY HAZESDR DXTA201804300887Cooling Fan · failedBEHIND LEFT PILOT SEAT, A LOUD SQUEALING NOISE STARTED FOR ABOUT 10+ MINS THEN FOLLOWED BY A STRONG BURNING ODOR IN THE MAIN CABIN. THEN IT QUIT. TROUBLESHOT AND FOUND AVIONICS COOLING FAN TO BE THE SOURCE OF THE SQUEALING AND BURNING ODOR. REMOVED AND REPL
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