- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 20536
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 24, 2014
- Certificate issued
- November 30, 2024
- Expires
- November 30, 2031
- Mode S code
- A752B3
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 N571FXMatched 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 N571FXMatched 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2020070600206Apu · odorOIL SMELL COMING THROUGH VENTS ON GROUND AND IN THE AIR. REMOVED AND REPLACED APU.SDR J7SA20190920001Engine · malfunctionedDIVERTED DUE TO LOUD BANG, AIRCRAFT SHUTTER, AND ENGINE 2 ROLL BACK WHILE PASSING THROUGH 10,000 FEET AT 250 KTS. AS #2 ENGINE ROLLED BACK. N2 INDICATED MAGENTA DASHES, N1 INDICATED 11%, R FADEC FAIL AMBER CAS. L&R AUX BUS OFF CYAN CAS PERFORMED SINGLE ENG LASDR J7SA20161205001Detector Loop · out of positionAIR TURNBACK DUE TO RT PACK LEAK CAS MESSAGE IN FLIGHT. CREW RAN MEMORY ITEMS AND CHECKLIST, DESCENDED TO 9,000 FT AND DEPRESSUREIZED. DECLARED AN EMERGENCY AFTER DESCENT. LANDED WITHOUT INCIDENT. INSPECTED BLEED AIR LEAK DETECTION LOOP. FOUND LOOP MT73P2 TO
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