# Falcon 2000LX

Source: https://jetatlas.ai/ko/aircraft/dassault-falcon-2000lx
Publisher: JetAtlas
Retrieved: 2026-10-27T19:32:13.884Z (not the data verification date)
Record updated: 2026-09-13T15:20:16.606Z
Verified: unknown
Published: not recorded
Requested language: ko
Field languages: {"description":"ko"}
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.

2009년 4월 인증을 받은 Falcon 2000LX는 2000EX EASy에 Aviation Partners 블렌디드 윙렛을 더해 승객 6명, 마하 0.80 기준 항속거리를 4,000해리로 늘렸습니다. 윙렛은 마하 0.80에서 연료 효율을 최대 5퍼센트 개선했으며, 초기 Falcon 2000용 개조 옵션으로도 제공되었습니다. 2014년 내측 슬랫을 더한 2000LXS가 뒤를 이었습니다.

```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": "2009년 4월 인증을 받은 Falcon 2000LX는 2000EX EASy에 Aviation Partners 블렌디드 윙렛을 더해 승객 6명, 마하 0.80 기준 항속거리를 4,000해리로 늘렸습니다. 윙렛은 마하 0.80에서 연료 효율을 최대 5퍼센트 개선했으며, 초기 Falcon 2000용 개조 옵션으로도 제공되었습니다. 2014년 내측 슬랫을 더한 2000LXS가 뒤를 이었습니다."
}
```

## 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/ko/aircraft/dassault-falcon-2000lx