- Registered owner
- Citation X Parts LLC
- Location
- Liberty, NC
- Owner type
- LLC
- Serial number
- 20150
- Year built
- 2007
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 31, 2007
- Certificate issued
- September 28, 2026
- Expires
- September 30, 2033
- Mode S code
- A6B4B7
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10Engine modelAmateur-built UNKNOWN ENG
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 54
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 | 3 |
| 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 N531FXMatched 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 N531FXMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2026031200476Acm · faultedREJECTED TAKEOFF DUE TO PACK TEMP HIGH CAS, PACK FAIL CAS, AND VISIBLE SMOKE IN CABIN. CREW TAXIED BACK TO THE FBO WITHOUT INCIDENT. FOUND BROKEN BLADE ON ACM. REPLACED ACM AND PRECOOLER. PERFORMED OPS AND BLEED CHECKS. ALL CHECKS SATISFACTORY AT THIS TIME. WOSDR J7SA2025111000460Acm · faultedBURNING SMELL ON DESCENT ACCOMPANIED BY VERY WARM AIR. AIRCRAFT LANDED WITHOUT INCIDENT AT KSSI. AFTER LANDING, CREW RECEIVED AMBER PACK TEMP HIGH CAS ON SYNOPTIC. REPLACED AIR CYCLE MACHINE. PERFORMED SUCCESSFUL OPS CHECK AND LEAK CHECK IAW CH 300 AMM 21-52-1SDR J7SA2021120200304Pump · failedNO FLAP LANDING DUE TO HYDRAULIC PUMP FAILURE. AIRCRAFT LANDED WITHOUT INCIDENT AT KOAK. AFTER LANDING, CREW NOTICED A PUDDLE OF HYDRAULIC FLUID ON GROUND. REPLACED DEFECTIVE RH HYDRAULIC SYSTEM FILTER MANIFOLD IAW CH 300 AMM 32-34-05. REPLACED DAMAGED O-RING SDR J7SA202002062001Screw · looseRIGHT LEADING EDGE HAS LOOSE SCREW ON MIDDLE LEADING EDGE PANEL. REMOVED AND REPLACED LOOSE SCREW PER BD100 AMM 57-41-09 P/N NAS8703-3.SDR J7SA20181230001Apu · odorINVESTIGATE OIL SMELL IN CABIN WITH APU RUNNING. PERFORMED BOROSCOPE INSP OF APU INLET. REPLACED APU.SDR J7SA2018053028001Fire Warning · false activationAPU FIRE CAS ILLUMINATED DURING CRUISE AT 10000 FEET. COMPLIED WITH QRH PROCEDURES AND DIVERTED. R & R THE APU SQUIB. INSPECTED APU ENCLOSURE AND FOUND NO EVIDENCE OF FIRE. NO DEFECTS NOTED. RESEALED FIREWALL.SDR J7SA2018091916001Screw · missingRIGHT LEADING EDGE OF WING MISSING ONE SCREW ON TOP OF WING NEAR WING ROOT. REMOVED RT INB LE FOUND NUT PLATE LOOSE IN GANG CHANNEL AT MISSING SCREW LOCATION RESECURED NUT PLATE IN GANG CHANNEL. DURING REMOVAL OF LE FOUND STRIPPED NUT PLATE BOLT AT RT INB LE BSDR J7SA2018091903001Nut Plate · out of positionON POST FLIGHT SCREW ON UPPER LEADING EDGE OF RIGHT WING FOUND PROTRUDING SCREW NOT ENGAGING ANYTHING WHEN ATTEMPT MADE TO TIGHTEN IT. REMOVED RT CENTER WING LEADING EDGE PANEL. LOCATED AND REINSTALLED NUT PLATE ON UPPER ATTACHING POINT, REINSTALLED RT CENTER SDR J7SA20171023001Generator · trippedAT 5000 FT, 200 KTS, ENGAGED APU STARTER AND BOTH GENERATORS TRIPPED OFF LINE. AFTER APU WAS RUNNING, RESET BOTH GENERATORS. AIRCRAFT LANDED WITHOUT INCIDENT. TIGHTENED LOOSE LT GENERATOR POWER TERMINAL AFTER REMOVING CORROSION. REMOVED CORROSION FROM RT GESDR J7SA20170719001Sensing Element · faultyFALSE FIRE WARNING: "APU FIRE TASK" ILLUMINATED WITH A TRIPLE CHIME AND APU FIRE AURAL WARNING. CREW FOLLOWED CHECKLIST, TURNED OFF APU AND USED NR 2 FIRE EXTINGUISHER. LANDED WITHOUT INCIDENT. PRELIM INSPECTION REVEALS NO SIGNS OF FIRE. REPLACED APU SENSING ESDR J7SA20151226001Shaft · shearedTURNED BACK TO BASE DUE TO GEN FAILURE. AN EMER WAS DECLARED & THE ACFT LANDED WITH NO FURTHER INCIDENT. FOUND THE RT GEN SHAFT SHEARED. THE SHAFT COUPLING WAS REPLACED & AN OVERHAULED GEN INSTALLED. LEAK & OPERATIONS CHECKS WERE GOOD & THE ACFT RETURNED T
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