- Registered owner
- Citation X Parts LLC
- Location
- Liberty, NC
- Owner type
- LLC
- Serial number
- 20118
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 17, 2008
- Certificate issued
- April 20, 2026
- Expires
- April 30, 2033
- Mode S code
- A69FCB
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 N526FXMatched 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 N526FXMatched 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 J7SA2026030200475Vhf Comm · smokeAIR TURN BACK DUE TO SMOKE IN CABIN DURING CLIMB BETWEEN 12000 AND 15000 FT. CREW NOTED THAT THE ODOR SEEMED TO BE COMING FROM BEHIND THE LT CIRCUIT BREAKER PANEL. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED THE NR 1 VHF 4000 IAW AMM 23-11-01. PERFORMEDSDR J7SA2019060729001Fire Warning · false activationDIVERTED DUE TO AN APU FIRE INDICATION RECEIVED INFLIGHT. COMPLIED WITH QRH PROCEDURE & APU FIRE INDICATION EXTINGUISHED. AIRCRAFT WAS AT 11,000' AND 260 KTS. [AIRCRAFT LANDED WITHOUT INCIDENT OR FIRE DAMAGE.] UNDER FURTHER INSPECTION FOUND MOUNTS NOT SEATEDSDR J7SA20190318001Fire Warning · false activationAS WE WERE CLIMBING UP AROUND 12000 FEET AND AT APPROX 280KT PNF WERE JUST ABOUT TO SWITCH OFF APU AS WE GOT A APU FIRE CAS AND MASTER CAUTION THAT CAME ON. AS THE SWITCH CAME TO OFF POSITION THE INIDICATION DISAPPEARED. PERFORMED GENERAL VISUAL INSPECTION OF SDR J7SA20170901001Fire Warning · false activationAPU FIRE CAS DISPLAYED IN FLIGHT. FOLLOWED QRH, BOTTLE NR 2 BLOWN. LANDED WITHOUT INCIDENT. INSPECTED APU ENCLOSURE FOR POSSIBLE APU FIRE. FOUND NO SIGNS OF ACTUAL APU FIRE. R & R NR 2 FIRE BOTTLE AND BOTH LOWER APU ENGINE MOUNT INSULATORS. OPS CHECKED THE FSDR J7SA20170730001Fire Warning · false activationAPU FIRE INDICATION, TURNED OFF APU, THERE WERE NO INDICATIONS OF ACTUAL FIRE. SECURED THE APU RT INDUCTOR LOOP HARNESS. OPS CHECKED GOOD AND NO FAULTS FOUND ON MDC OR CAS. THE INDUCTOR LOOP IS NOT BELIEVED TO BE THE CAUSE OF THE FALSE FIRE WARNING. IT IS BSDR J7SA20170715001Control Unit · malfunctionedDIVERTED DUE TO RED "APU FIRE" CAS POSTED AFTER TAKEOFF. CREW DEPRESSED APU FIRE SWITCH AND EXT BUTTON. THERE WERE NO FURTHER INDICATIONS OF FIRE. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION REVEALS NO EXTERIOR OR INTERIOR SIGNS OF FIRE OR DAMAGE. REPLACED FSDR J7SA01082011001O-Ring · deformedAFTER DEPARTURE, RT (NR2) "PRESSURE LOW" CAS MESSAGE POSTED WHILE CLIMBING THROUGH FL200. HYD SYNOPTIC PAGE SHOWED PRESSURE DROPPING TO O PSI WITHIN 1 MINUTE AND 0 PERCENT QUANTITY FOR NR 2 HYD SYS. CREW DECLARED EMERGENCY AND ACFT WAS DIVERTED AND HAD AN UNE
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