- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 20278
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 31, 2010
- Certificate issued
- October 30, 2019
- Expires
- October 31, 2029
- Mode S code
- A6EC95
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 N545XJMatched 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 N545XJMatched 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 U5QA202602020166Dcpc · failedCREW REPORTS A CYAN ELECTRICAL FAULT FOLLOWED BY BATTERIES AND GENERATORS DROPPING OFFLINE. THE ELECTRICAL PANEL KEPT FLICKERING ON AND OFF. REMOVED AND REPLACED LEFT DC POWER CENTER IAW AMM 24-61-01. COMPLIED WITH BOMBARDIER RIL BD-0069-GENERATOR LOAD TESSDR U5QA2024010940143Pump · failedRT HYD TEMP HIGH , ASSOCIATED WITH THE HYD ENG PUMP FAIL. EMERGENCY DECLARED. MX C/A: VERIFIED THE RH EDP FAILED CARRIED OUT THE GVI OF THE EDP AFTER DRY OPERATION. VERIFIED THE RH EDP FAILED IRW CL 300 AMM 05-51-29. REMOVED AND REPLACED THE RIGHT HAND EDP. RSDR U5QA202409280138Clamp · faultedDURING MX CK FLT FOLLOWING 7500L INSP, LEFT PYLON BLEED LEAK (RED CAS MESSAGE). MX C/A: LEFT PYLON BLEED LEAK (RED CAS MESSAGE). REPLACED 2 EA NEW E-SEALS AND 2 EA NEW V BAND CLAMPS LH INTERMEDIATE VALVE IAW CL 300-AMM 36-11-05-000-801, 36-11-00-790-801 AND 3SDR AWKA20220226001None · noneWHILE AT ALTITUDE, FLIGHT CREW RECEIVED A CYAN "R ENG HYD PUMP FAIL" CAS MESSAGE AND 0% QUANTITY SHOWING ON THE RH HYDRAULIC SYSTEM. CREW RAN THE APPROPRIATE CHECKLIST AND DECLARED AN EMERGENCY WITH ATC. AFTER CONSULTING WITH MX CONTROL, THE DECISION WAS MADE SDR AWKA2021081401Microwave Oven · faultedSHORTLY AFTER THE CABIN ATTENDANT USED THE GALLEY MICROWAVE OVEN, THE OVEN TURNED ITSELF ON UN-COMMANDED. THIS ACTIVATION WENT UN-NOTICED AND BEGAN TO BURN THE REMAINING FOOD WITHIN. A FEW MINUTES AFTER, THE CABIN ATTENDED BEGAN TO SMELL SMOKE AND NOTIFIED THESDR AWKA2021020201Acm · seizedWHILE CLIMBING OUT AND APPROXIMATELY 1000 FEET AGL, A PASSENGER REPORTED SMOKE IN THE CABIN TO THE FLIGHT CREW. FLIGHT CREW CONFIRMED WHAT TO BE SMOKE. AN-IN FLIGHT EMERGENCY WAS DECLARED AND THE CREW RETURNED TO THE AIRFIELD. FIRE CREWS WERE REQUESTED AND AN SDR AWKA20191227001Pseu · failedWHILE EN ROUTE, FLIGHT CREW RECEIVED AN AMBER WOW FAIL AND CYAN PROX SYS FAIL CAS MESSAGES. AFTER DISCUSSION WITH MX CONTROL, CREW ELECTED TO CONTINUE ON TO BED AND DECLARED AN EMERGENCY WITH APPROACH CONTROL, ADVISING THEM THAT THEY MAY NOT HAVE SUFFICIENT DISDR AWKA2019022001Carbon Seal · failedTHE MANUFACTURER ADVISED THAT THEY HAD OBSERVED UNUSUAL AND SUDDEN SHIFTS IN OIL PRESSURE INDICATIONS, ALTERNATING BETWEEN POSITIVE AND NEGATIVE READINGS. THE MANUFACTURER ADVISED THAT THE CARBON SEAL SHOULD BE ACCESSED FOR IMMEDIATE INSPECTION. THE AIRCRAFT W
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