Overview including differentiating features from other aircraft in its category
The Falcon 2000LXS was designed as a replacement for its predecessor, the Falcon 2000LX. One of the biggest differentiating features of the 2000LXS is the model’s improved short field capability. The reduced landing distance allows for more airports to open up compared to other aircraft in its class.
As of February 2015, the Falcon 2000LXS market is comprised of 6% pre-owned. The percentage for sale is 10.5% with 50% under an exclusive broker agreement and average days on the market are 46 days.
Brief History
The Falcon 2000LXS debuted in 2014. There have been a total of 23 aircraft produced with 19 currently in operation.
Worldwide Appeal
Of the 19 Falcon 2000LXS in operation by continent, North America has 63%, followed by Europe at 25% for a combined total of 88%. There is only one company (International Paper Company) having a 2 aircraft fleet, the others are all single aircraft owners and operators. Additionally, only one of the Falcon 2000LXS jets is leased.
Highlights
Performance
The Falcon 2000LXS is powered by two Pratt and Whitney Canada PWC308C engines each offering 7,000 pounds of thrust. The Falcon 2000LXS uses 238 gallons per hour (GPH). The range of the Falcon 2000LXS is 4,075 nm operating under NBAA IFR 4 passengers with available fuel.
Interior
The cabin volume for the Falcon 2000LXS is 1,024 cubic feet. Typical configuration features 8 passenger and 2 crew seats.
Design
The Falcon 2000LXS Maximum Take-Off Weight (MTOW) is 42,800 pounds with a maximum range of 4,145 nm.
Speed
| Maximum Cruise Speed: | 482 kts | 893 km/h | ||||||
| Long-range Speed: | 437 kts | 809 km/h |
Airfield Performance
| Takeoff distance: | 4,675 ft (1,425 m) | (SL, ISA, MTOW) | ||||||
| Landing distance: | 2,300 ft (701 m) | (SL, ISA, MLW) |
Operating Altitude
| Maximum operating altitude: | 47,000 ft (14,326 m) |
Noise Level (EPNdB)
| Takeoff: | 76.4 | Approach: | 90.5 | Lateral: | 91.7 |
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Weights
| A. | Maximum ramp weight: | 43,000 lb (19,504 kg) | ||||||
| B. | Maximum takeoff weight: | 42,800 lb (19,414 kg) | ||||||
| C. | Maximum landing weight: | 39,300 lb (17,826 kg) | ||||||
| D. | Maximum zero fuel weight: | 29,700 lb (13,472 kg) | ||||||
| E. | Standard basic operating weight: | 24,750 lb (11,226 kg) |
Avionics
Honeywell Primus Epic-based EASy II
Resources
Contact Us at +1 919 941 8400 or [email protected] to request a custom range report including detailed aircraft comparisons.
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