- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 20095
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 24, 2008
- Certificate issued
- March 25, 2019
- Expires
- March 31, 2029
- Mode S code
- A6985D
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 N524FXMatched 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 N524FXMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA20190222001Dcpc · malfunctionedDIVERTED DUE TO MULTIPLE OCCURRENCE'S OF "L BAT FAIL, L GEN FAIL" AND/OR "R BAT FAIL, R GEN FAIL" CAS MESSAGES. AIRCRAFT LANDED WITHOUT INCIDENT. R&R LT DCPC WITH A REPAIRED UNIT.SDR J7SA20180127001Bracket · crackedAPU FIREWALL LOWER AND LEFT BRACKETS CRACKED. R & R THE BRACKETS.SDR J7SA20170805001Control Valve · failedLEFT SIDE BRAKES WOULD ENGAGE ON LANDING BUT THEN STOPPED WORKING FOR 1-2 SECONDS AROUND 60 KTS AND 15-20 KTS. R & R BRAKE CONTROL VALVE. LEAK CHECKED GOOD BUT LH BRAKES STILL FAILED DURING TAXI CHECK. R&R BRAKE CONTROL UNIT WITH MODIFIED UNIT. LEAK CHECKED GSDR J7SA20160726001Safety Valve · malfunctionedEXPERIENCED RAPID CABIN DEPRESSURIZATION AT FL430 CABIN ALTITUDE INCREASED AT 10,000+ FEET PER MINUTE. EXECUTED EMERGENCY DESCENT TO 15,000 FT IN LESS THAN 4 MINUTES. AFTER LEVELING AT 15,000 FT CABIN PRESSURE SYSTEM APPEARED TO RETURN TO NORMAL OPERATION AND SDR J7SA20120315001Element · out of positionRIGHT BLEED LEAK RED CAS POSTED AFTER TAKEOFF. ACFT DIVERTED. REPOSITIONED SENSING ELEMENT AND CLAMPS.SDR 3002009512280Structure · damagedBIRD STRIKE HIT LT HORZ STAB AND VERTICAL STAB, LEADING EDGE FOR THE LT STAB, LEADING EDGE ACCESS PANEL, UPPER AND LOWER HORSE COLLAR DAMAGED. NO DAMAGE FOUND TO STAB ACTUATOR. FOUND BIRD PARTS INSIDE PANELS.
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