- Registered owner
- Citation X Parts LLC
- Location
- Liberty, NC
- Owner type
- LLC
- Serial number
- 20211
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 18, 2008
- Certificate issued
- February 19, 2026
- Expires
- February 28, 2033
- Mode S code
- A6DC36
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 N541FXMatched 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 N541FXMatched 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 J7SA2023062900362Unknown · unknownNUT SHEARED DURING INSTALLATION OF R/H MLG SIDE STAY ACTUATOR PIN. REPLACED R/H MLG SIDE STAY OB ATTACH PIN. AS A PRECAUTION, REPLACED THE L/H MLG SIDE STAY ACTUATOR OB ATTACH PIN. WORK COMPLETED IAW CL 300 AMM 32-32-07-400-801.SDR J7SA2020010304003Screw · missingRIGHT MID LEADING EDGE UPPER MISSING SCREW AND NUTPLATE.COMPLIED WITH CH 300 LEADING EDGE MISSING FASTENER TEMP0RARY REPAIR IRT AQRD DOCUMENT REF # 911387-FS IR (DMH)SDR J7SA2020010304002Screw · missingRIGHT OUTBOARD LEADING EDGE MISSING SCREW AND NUT PLATE.COMPLIED WITH CH 300 LEADING EDGE MISSING FASTENER TEMP0RARY REPAIR IRT AQRD DOCUMENT REF # 911387-FS IR (DMH)SDR J7SA2020010304001Screw · missingLEADING EDGE UPPER L/H MISSING SCREW AND NUT PLATE.COMPLIED WITH CH 300 LEADING EDGE MISSING FASTENER TEMP0RARY REPAIR IRT AQRD DOCUMENT REF # 911387-FS IR (DMH)SDR J7SA2019102218001Line · failedLH (#1) HYDRAULIC SYSTEM FAILURE AFTER #1 ENGINE STARTED EICAS L HYD PRESS LOW AMBER HYD QUANTITY WENT TO 0% FLUID ON GROUND REMOVED AND REPLACED THE LINE AND C/W BLEEDING OF THE # 1 HYD SYSTEM OPERATED THE SYSTEM NO FURTHER LEAKS OR DEFECTS NOTEDSDR J7SA20160307001Fitting · leakingEMERGENCY DECLARED DUE TO LT HYD LOW, CAS MESSAGE ON INITIAL DESCENT. LOST PRESSURE WHEN ATTEMPTING TO LOWER GEAR, USED THE MANUAL EXTENSION. LANDED WITHOUT INCIDENT. LARGE LEAK FROM LT PRESS FILTER MANIFOLD FITTING. RESEATED LINE & UNION, NO LEAKS DETECTSDR J7SA20151019001Pump · failedON DESCENT, A LOUD RUMBLING NOISE OCCURRED TOWARDS THE REAR OF THE ACFT & A LT HYD LOW MSG APPEARED. FOLLOWED THE APPROPRIATE CHECKLIST, MANUALLY LOWERED THE MLG, & PROCEEDED TO THE LAND THE ACFT NORMALLY. NOSE GEAR STEERING WAS INOPERATIVE, BUT THEY MANAGED
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