# Falcon 2000LX

Source: https://jetatlas.ai/ja/aircraft/dassault-falcon-2000lx
Publisher: JetAtlas
Retrieved: 2026-10-27T10:17:31.143Z (not the data verification date)
Record updated: 2026-09-13T15:20:16.606Z
Verified: unknown
Published: not recorded
Requested language: ja
Field languages: {"description":"ja"}
Terms: CC BY 4.0 — https://creativecommons.org/licenses/by/4.0/

- Published specifications depend on configuration. Prices and operating costs are editorial estimates, not quotations.
- Range and runway figures do not establish operational suitability.

2009年4月に型式証明を取得したFalcon 2000LXは、2000EX EASyにAviation Partnersのブレンデッドウィングレットを加え、乗客6名、Mach 0.80での航続距離を4,000 nmに延ばしました。ウィングレットはMach 0.80で燃費を最大5パーセント改善し、初期のFalcon 2000向けのレトロフィットとしても提供されました。2014年には内側スラットを加えた2000LXSに引き継がれました。

```json
{
  "kind": "aircraft",
  "slug": "dassault-falcon-2000lx",
  "name": "Falcon 2000LX",
  "manufacturer_slug": "dassault",
  "manufacturer_name": "Dassault Aviation",
  "category": "large",
  "status": "out-of-production",
  "first_delivery_year": 2009,
  "production_end_year": 2014,
  "price_new_usd_m": 32.1,
  "preowned_low_usd_m": 14,
  "preowned_high_usd_m": 19,
  "range_nm": 4000,
  "max_cruise_kts": 482,
  "max_mach": 0.862,
  "max_altitude_ft": 47000,
  "passengers_typical": 8,
  "passengers_max": 10,
  "cabin_length_ft": 26.2,
  "cabin_width_ft": 7.7,
  "cabin_height_ft": 6.2,
  "cabin_volume_cuft": 1024,
  "baggage_cuft": 131,
  "mtow_lb": 42200,
  "takeoff_distance_ft": 5585,
  "landing_distance_ft": 2630,
  "engines": "2 × Pratt & Whitney Canada PW308C",
  "engine_count": 2,
  "fuel_burn_gph": 264,
  "hourly_variable_cost_usd": 3600,
  "annual_fixed_cost_usd": 1050000,
  "crew": 2,
  "length_ft": 66.3,
  "wingspan_ft": 70.2,
  "height_ft": 23.2,
  "max_payload_lb": 5425,
  "max_fuel_lb": 16660,
  "engine_thrust_lbf": 7000,
  "engine_shp": null,
  "cabin_altitude_ft": null,
  "avionics": "Dassault EASy (Honeywell Primus Epic)",
  "description": "2009年4月に型式証明を取得したFalcon 2000LXは、2000EX EASyにAviation Partnersのブレンデッドウィングレットを加え、乗客6名、Mach 0.80での航続距離を4,000 nmに延ばしました。ウィングレットはMach 0.80で燃費を最大5パーセント改善し、初期のFalcon 2000向けのレトロフィットとしても提供されました。2014年には内側スラットを加えた2000LXSに引き継がれました。"
}
```

## References
- https://web.archive.org/web/20160713085611/http://compair.aviationresearch.com/database_files/TheImage_513.pdf
- https://web.archive.org/web/20080531155247/http://www.dassaultfalcon.com:80/aircraft/2000lx/specs.jsp
- https://web.archive.org/web/20081202180504/http://www.dassaultfalcon.com/aircraft/2000lx/performance.jsp
- https://web.archive.org/web/20080521012155/http://www.dassaultfalcon.com:80/aircraft/2000lx/
- https://www.easa.europa.eu/en/downloads/7510/en
- https://www.bjtonline.com/business-jet-news/dassaults-falcon-2000s
- https://aviationweek.com/business-aviation/aircraft-propulsion/20twenty-continuously-improved-falcon-2000
- https://en.wikipedia.org/wiki/Dassault_Falcon_2000

Methodology: https://jetatlas.ai/en/methodology
Cite: JetAtlas, https://jetatlas.ai/ja/aircraft/dassault-falcon-2000lx