- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 20213
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 6, 2008
- Certificate issued
- October 31, 2019
- Expires
- October 31, 2029
- Mode S code
- A6CC84
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-1-1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 57
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 | 6 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 3 |
| 2021 | 6 |
| 2022 | 5 |
| 2023 | 9 |
| 2024 | 9 |
| 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 N537XJMatched 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 N537XJMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR U5QA202306300116Unknown · unknownL ENG EXCEEDANCE ON EICAS IIN FLIGHT AT FL 450. ITT THRESHOLD EXCEEDANCE. STRONG CONTINIOUS VIBRATIONS AND STRONG CONTINIOUS SHAKING OF THE AIRCRAFT. COMPLETED QRH AND ENDED UP SHUTTING THE ENGINE DOWN IN FLIGHT. DECLARED EMERGENCY AND LANDED SINGLE ENGINE. MSDR U5QA202306010115Acm · smokeON TAKEOFF POWER APPLIED, SMELL OF GUN POWDER SMOKE WAS APPAREMT, VISIBLE LIGHT SMOKE WAS APPARENT, AND WE ABORTED TAKEOFF RUN IMMEDIATLY. AFTER POWER REDUCRION SMOKE INTENSITY FELL. UPON ENGINE SHUTDOWN NO INDICATIONS OF ANY SMOKE OR SMELL. ONCE APU AIR CONDISDR AWKA201705170001Warning System · false activationDURING CRUISE AT FL450, FLIGHT CREW RECEIVED AN AMBER WOW FAIL AND CYAN PROX SYSTEM FAULT CAS MESSAGES. CREW RAN THE RESPECTIVE CHECKLIST, CONSULTED WITH MX CONTROL AND ELECTED TO CONTINUE TO THEIR ORIGINALLY SCHEDULED DESTINATION. AN EMERGENCY WAS DECLARED TOSDR AWKA201605050001Safety Valve · failedWHILE AT FL450, FLIGHT CREW RECEIVED A "RED" CABIN ALT WARNING HIGH CAS MESSAGE, ALONG WITH A MASTER CAUTION WARNING AND AURAL ALERT. THE CREW DONNED THEIR O2 MASKS; DEPLOYED THE PAX O2 MASKS AND IMMEDIATELY BEGAN AN EMERGENCY DESCENT. CREW INFORMED ATC THATSDR AWKA20160226001Acm · seizedDURING TAKEOFF, THE FLIGHT CREW NOTICED WHAT SEEMED TO BE AN ELEC SMELL ALONG WITH SMOKE IN THE CABIN. THE CREW LEVELED OFF AT 2000’ & THEN RETURNED TO FIELD, WHILE DOING SO THEY TURNED THE AIR SOURCE OFF & RAM AIR ON, THIS QUICKLY CLEARED THE SMOKE. AN UNEVSDR AWKA201304020213Control Unit · failedENROUTE, FLIGHT CREW RECEIVED A WEIGHT ON WHEELS AND A PROXIMITY SENSOR FAIL CAS MESSAGE. REFERENCED QRH AND CONTACTED MAINTENANCE CONTROL. IT WAS DETERMINED THAT NORMAL GROUND SPOILER, NOSE WHEEL STEERING, AND NORMAL BRAKING COULD BE COMPROMISED AFTER TOUCHDSDR AWKA537702Selector Valve · faultyON APPROACH, THE LANDING GEAR FAILED TO EXTEND WHEN THE FLIGHT CREW SELECTED LANDING GEAR TO THE DOWN POSITION. A (SYS PROX FAULT) MESSAGE WAS RECEIVED FOLLOWED BY A (GEAR DISAGREE FAULT) MESSAGE. THE GEAR DISAGREE CHECKLIST WAS PERFORMED ALONG WITH SOME TROUB
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