- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 20112
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 20, 2006
- Certificate issued
- February 12, 2019
- Expires
- February 28, 2029
- Mode S code
- A69C14
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 N525FXMatched 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 N525FXMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2020102600231Engine · vibrationAIR TURN BACK DUE TO VIBRATIONS IN LEFT ENGINES AT FL 220. CREW EXPERIENCED VIBE IN YOKE AND PEDALS, AND INTENSITY WOULD INCREASE WHEN ADDING POWER. AIRCRAFT LANDED WITHOUT INCIDENT AT KHPN. REMOVED AND REPLACED NR 1 ENGINE, IAW AMM 71-00-01.SDR J7SA2019022213001Pump · seized2000 FT GEAR AND FLAPS 20 SELECTED LOUD NOISE AND VIBRATION AND LEFT HYD PRES LOW CAS MESSAGE ILLUMINATED HAPPENED SIMULTANEOUSLY AMBER LEFT HYD PRESS LOW CHECKLIST PERFORMED INCLUDING LG PULL HANDLE PULLED. [LOSS OF NOSE WHEEL STEERING ON THE RUNWAY.] AIRCRAFSDR J7SA0411201401Control Module · dirtyRED ESS POWER ONLY, AMBER RT GEN FAIL, AMBER RT BATTERY FAIL & CYAN ELEC FAULT, ILLUMINATED. LANDING & TAXI WERE UNEVENTFUL. THE FLIGHT WAS ON A PART 91 RELEASE NR 91FJ1325. PERFORMED THOROUGH CLEANING OF LT & RT DCPC. PERFORMED OPERATIONS CHECK OF ELEC SDR J7SA20120320001Safety Valve · failedAT 43K ALTITUDE, ACFT RAPIDLY DECOMPRESSED TO 15K FT. REPLACED LT SAFETY VALVE.
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