- Owner type
- Co-owned, fractional ownership
- Serial number
- 20646
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 28, 2016
- Certificate issued
- April 10, 2026
- Expires
- April 30, 2033
- Mode S code
- AACFBE
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 N796QSMatched 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 N796QSMatched 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 DXTA2026071708804Engine · vibrationAT CRUISE AT FL400 FELT A VIBRATION IN PLANE. ABOUT A MIN LATER L ENG VIBRATION CASS MESS CAME ON. WHILE PULLING OUT QRH, RECEIVED A LT ITT EXCEEDANCE WARNING. BEGAN SMELLING SMOKE IN CABIN. PUT ON O2 MASK. RECEIVED A LT ENG FLAMEOUT CASS MESSAGE NEXT. RAN QRSDR DXTA2025091904993Door · lack of lubeDURING OUR FIRST FLIGHT OF THE DAY, WHEN WALKING UP TO THE AIRCRAFT AND ATTEMPTING TO OPEN THE MAIN CABIN DOOR, THE DOOR HANDLE WOULD LIFT UP SLIGHTLY AND THEN BECOME STUCK. WE COULD NOT MOVE IT ANY FURTHER AND WE WERE AFRAID THAT BY APPLYING MUCH MORE PRESSUSDR DXTA2025082204650Precooler · leakingIN FLIGHT CLIMBING FROM 29000 TO 35000 FT WE SMELLED AN ELECTRICAL BURNING TYPE SMELL AND HAD A RED CAS MSG PACK LEAK. WE RAN THE QRH CHECKLIST AND GOT A A/C TEMP HI AMBER CAS. WE LANDED WITHOUT EVENT. I BELIEVE THIS IS A REPEAT WRITE UP. WHILE AIRCRAFT PRESSUSDR DXTA2025070204085Trim System · faultedIN CRUISE AT FL260 AND 310KTS. EXCESSIVE RIGHT WING TRIM REQUIRED FOR STRAIGHT AND LEVEL. AT LOWER ALTUTUDE AND SLOWER SPEEDS LESS RIGHT AILERON TRIM REQUIRED PERFORMED RIGGING OF THE LH AILERON BALANCE GEARED-TAB IN REFERENCE TO AMM 27-11-21-220-801. ADJUSTEDSDR DXTA2025052003529Mcu · defectiveAMBER PRI STAB TRIM FAIL CAS MESSAGE ILLUMINATED AT APPROXIMATELY 4000' AND 10MILES FROM THE AIRPORT ON AN APPROACH. A SLIGHT NOSE DOWN PRESSURE WAS FELT ONCE AP WAS DISCONNECTED. NO ISSUES WITH SECONDARY SELECTED. REPLACED MCU IAW CL-350 AMM 27-41-13. OPS CSDR DXTA2025012202019Selector Valve · faultedREPEAT WRITE-UP. AFTER DEPARTURE AND SELECTED GEAR UP EVERTHING SOUNDED NORMAL EXCEPT THE NOSE GEAR WAS SHOWING UP AND THE LEFT AND RIGHT MAIN LANDING GEAR ANNUNCIATORS WERE SHOWING GREEN DOWN AND LOCKED. THEN WE RECEIVED THE AMBER GEAR DISAGREE CASS MESSAGE. SDR DXTA2025012001970Pseu · faultedRIGHT MLG LANDING GEAR RETRACTION: AFTER DEPARTURE AND SELECTED THE GEAR UP . EVERYTHING SOUNDED LIKE A NORMAL GEAR RETRACTION, HOWEVER ONLY THE NOSE GEAR WAS SHOWING UP WITH BOTH THE LEFT AND RIGHT LANDING GEAR ANNUNCIATORS INDICATING GREEN DOWN AN LOCKED,SDR DXTA2024112101164Sign · damagedLAV EXIT SIGN/LIGHT: LIGHTED LAVATORY "EXIT" SIGN DOES NOT ILLUMINATE WHEN THE REST OF THE INTERIOR EMERGENCY LIGHTS ARE ON. REMOVED AND REPLACED AFT LAV EXIT SIGN IAW CL350 SMM TASK 33-51-05-400-801 REV1 COMPLIED WITH OPS OF EXIT SIGN IAW CL350 SMM TASK 33-50
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