Product Overview
Dassault launched the Falcon 900 in 1987 and introduced the Falcon 900EX in 1996. In 2003 Dassault began offering the 900EX with the EASy digital cockpit calling the model the 900EX EASy. Based on the Honeywell Primus Epic system, EASy (Enhanced Avionics System) offers improved safety via information management features to improve overall crew situational awareness.
As of September 2024, 96.7% of Falcon 900EX EASy ownership comes from the pre-owned market, the other 3.3% from new. 7 of those are currently for sale with the majority (57%) under an exclusive broker agreement. For those on the market, the average sale time is 292 days.
Brief History
The Falcon 900EX EASy received certification from the FAA and EASA in November 2003 and production ended in 2010. A total of 122 Falcon 900EX EASy business jets were built, 3 are inactive.
Worldwide Appeal
There are 113 Falcon 900EX EASy business jets in operation today. All of these are wholly owned. 12.6% are currently leased. North America has the largest percentage of Falcon 900EX EASy aircraft (76,1%), followed by West Europe (8,8%). TVPX Aircraft Solutions Inc. owns the largest fleet of Falcon 900 EX Easy business jets with 5.
Highlights
Interior
The cabin volume for the Falcon 900EX EASy is 1,264 cubic feet. Typical configuration features 12 passenger and 2 crew seats.
Performance
Three Honeywell TFE731-60 engines power the Falcon 900EX EASy each offering 5,000 pounds of thrust and using a combined 267 gallons per hour (GPH). The range of the Falcon 900EX EASy is 4,475 nm operating under NBAA IFR 4 passengers with available fuel.
Speed
| Maximum Cruise Speed: | 482 kts | 893 km/hr | ||
| Long-Range Speed: | 430 kts | 796 km/h |
Airfield Performance
| Takeoff distance: | 5,640 ft (1,719 m) |
(SL, ISA, MTOW)
|
||
| Landing distance: | 2,365 ft (721 m) |
(SL, ISA, MLW)
|
Operating Altitude
| Maximum operating altitude: | 51,000ft (15,545 m) |
Noise Level (EPNdB)
| Flyover: | 90.5 |
|---|---|
| Approach: | 92.3 |
| Takeoff: | 79.8 |
Weights
| A. | Maximum ramp weight: | 48,500 lb (21,999 kg) | ||
| B. | Maximum takeoff weight: | 48,300 lb (21,909 kg) | ||
| C. | Maximum landing weight: | 42,000 lb (19,051 kg) | ||
| D. | Maximum zero fuel weight: | 30,864 lb (14,515 kg) | ||
| E. | Standard basic operating weight: | 26,000 lb (11,793 kg) |
Range Report
Contact Us at +1 919 941 8400 or [email protected] to request a custom range report including detailed aircraft comparisons.
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