# Falcon 900B

Source: https://jetatlas.ai/es/aircraft/dassault-falcon-900b
Publisher: JetAtlas
Retrieved: 2026-10-27T20:41:18.774Z (not the data verification date)
Record updated: 2026-09-13T15:20:16.606Z
Verified: unknown
Published: not recorded
Requested language: es
Field languages: {"description":"es"}
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.

El Falcon 900B fue la actualización de 1991 del trirreactor Falcon 900 original de Dassault, con motores TFE731-5BR de 250 lb más de empuje cada uno y un alcance ampliado a unas 4,000 nm. Conservó la cabina de 7 ft 8 in de anchura y el techo de 51,000 ft del 900, y los Falcon 900 anteriores podían llevarse al estándar B mediante un boletín de servicio. La producción continuó hasta 1999, cuando ocupó su lugar el 900C equipado con Primus 2000.

```json
{
  "kind": "aircraft",
  "slug": "dassault-falcon-900b",
  "name": "Falcon 900B",
  "manufacturer_slug": "dassault",
  "manufacturer_name": "Dassault Aviation",
  "category": "large",
  "status": "out-of-production",
  "first_delivery_year": 1991,
  "production_end_year": 1999,
  "price_new_usd_m": 26,
  "preowned_low_usd_m": 5.7,
  "preowned_high_usd_m": 6.5,
  "range_nm": 4000,
  "max_cruise_kts": 500,
  "max_mach": 0.87,
  "max_altitude_ft": 51000,
  "passengers_typical": 12,
  "passengers_max": 19,
  "cabin_length_ft": 33.2,
  "cabin_width_ft": 7.7,
  "cabin_height_ft": 6.2,
  "cabin_volume_cuft": 1270,
  "baggage_cuft": 127,
  "mtow_lb": 45500,
  "takeoff_distance_ft": 5144,
  "landing_distance_ft": 3633,
  "engines": "3 × Honeywell TFE731-5BR-1C",
  "engine_count": 3,
  "fuel_burn_gph": 328,
  "hourly_variable_cost_usd": 4200,
  "annual_fixed_cost_usd": 1000000,
  "crew": 2,
  "length_ft": 66.3,
  "wingspan_ft": 63.4,
  "height_ft": 24.8,
  "max_payload_lb": 2945,
  "max_fuel_lb": 19165,
  "engine_thrust_lbf": 4750,
  "engine_shp": null,
  "cabin_altitude_ft": null,
  "avionics": null,
  "description": "El Falcon 900B fue la actualización de 1991 del trirreactor Falcon 900 original de Dassault, con motores TFE731-5BR de 250 lb más de empuje cada uno y un alcance ampliado a unas 4,000 nm. Conservó la cabina de 7 ft 8 in de anchura y el techo de 51,000 ft del 900, y los Falcon 900 anteriores podían llevarse al estándar B mediante un boletín de servicio. La producción continuó hasta 1999, cuando ocupó su lugar el 900C equipado con Primus 2000."
}
```

## References
- https://www.bjtonline.com/business-jet-news/dassault-falcon-900b
- https://www.bjtonline.com/sites/bjtonline.com/files/pdfs/falcon_900b_specs.pdf
- https://www.biobor.com/wp-content/uploads/2021/02/A46EU.pdf
- https://www.easa.europa.eu/en/downloads/7401/en
- https://aviationweek.com/business-aviation/aircraft-propulsion/20twenty-falcon-900-trijet-remains-popular
- https://www.avbuyer.com/aircraft/private-jets/dassault-falcon/900b
- https://web.archive.org/web/20020512115747/http://www.dassaultfalcon.com:80/aircraft/900c/specs.jsp
- https://en.wikipedia.org/wiki/Dassault_Falcon_900

Methodology: https://jetatlas.ai/en/methodology
Cite: JetAtlas, https://jetatlas.ai/es/aircraft/dassault-falcon-900b