2000 FALCON 900EX E&V ID A DASSAULT FALCON 900EX (F900) ASKING PRICE: US$ 10,995,000 YOM 2000 MSN ISSUE Page 1

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1 DASSAULT FALCON 900EX (F900) ASKING PRICE: US$ 10,995,000 YOM 2000 MSN 0054 Dassault, a company known for having high standards of engineering, structural quality, and technological advancement, made an impact on the heavy-iron private jet market with the Falcon 900. Ten years later, they improved an already-great private jet and introduced the Falcon 900EX. The cabin of the Falcon 900EX is huge. It is 6.1 feet high, 7.7 feet wide, 39 feet long (not including the cockpit), and has a total volume of 1,264 cubic feet. Standard seating is between eight and twelve passengers in a double-club configuration and a three-person divan. Two seats can be reclined and combined to make a full-length bed. Otherwise all of the seats are fully adjustable, can move along a track, swivel, recline, and everything else a seat could feasibly do. Console tables come standard, and there is room for virtually any piece of equipment computer, copier, scanner, TV, desk, and so on. Even with the tables and seats, there is plenty of room to walk around the cabin. The full-sized galley can be configured with equipment for hot meal preparation, including a hightemperature oven, microwave and the ubiquitous coffee maker. There are many interior configuration options, from wheelchair access to partitioned rooms. These separate rooms have been used to create a private office (with a full-sized desk) or a bedroom (with a queen-sized bed). The aft baggage compartment, which holds 127 cubic feet of baggage, is pressurized and air conditioned, and can be accessed in-flight. Sound levels within the cabin are very low, and temperature distribution is even throughout all parts of the cabin. ISSUE Page 1

2 The Falcon 900EX can take off in 5,213 feet at sea level (or at 7,214 feet at an altitude of 5,000 feet and a temperature of 77 F) due in part to its three (not two) Honeywell TFE engines. They are flat-rated to 5,000 pounds of thrust apiece (500 pounds more than the Falcon 900). The improved runway performance of the Falcon 900EX at high elevations and hot temperatures is remarkable. The Falcon 900 s runway requirement increases by 52% at high elevations and temperatures. (The runway requirement of a similar private jet, the Challenger 601-3R, increases by 83% under the same conditions.) Whereas the Falcon 900EX s runway requirement increases by only 38%. The Falcon 900EX s short runway performance is also due to its very light, tough frame. It is made of titanium, Kevlar, and carbon fiber composites, all of which are very lightweight but sturdy materials that allow the Falcon to do what much heavier private jets with more powerful engines can. The Falcon 900EX can fly a long-range mission of 4,940 miles (4,300 nautical miles) at.75 Mach, or a 4,480 mile (3,900 nautical miles) high-speed trip at.85 Mach. Its maximum range is 5,180 miles (4,500 nautical miles). It can cruise at altitudes as high as 51,000 feet and is rated to 9.3 psi, meaning it maintains a sea level cabin at 25,300 feet. Dassault opted for a Rockwell/Collins avionics system. It comes standard with dual Honeywell/Sperry WR-800 Flight Management System (FMS), Inertial Reference System, and Air- Data systems. A Smiths standard magnetic compass, emergency attitude gyro and dual Baker M-1045 audio systems also come standard. No matter how you look at it, the Dassault Falcon 900EX is an impressive private jet. With ranges of over 5,000 miles, an incredibly comfortable cabin, and an innovative three-engine configuration, it is an enviable machine. It is ideal for transoceanic and transcontinental trips and offers great versatility in flight planning. ISSUE Page 2

3 GENERAL CHARACTERISTICS Capacity: 14 passengers Length: 66 ft 4 in (20,22 m) Wingspan: 63 ft 5 in (19,33 m) Height: 24 ft 10 in (7,57 m) Max. Range: 4,500Nm ( km) Max Altitude: 51,000 ft ( m) Long Range Cruise: 436 kts (807 km/h) High Speed Cruise: 474 kts (878 km/h) Max. Certified Taxi Gross Weight: 48,500 Pounds ( kg) Max. Certified Take-Off Weight: 48,300 Pounds ( kg) Max. Certified Landing Weight: 42,000 Pounds ( kg) Basic Empty Weight: 26,000 Pounds ( kg) Maximum Zero Fuel Weight: 30,865 Pounds ( kg) Fuel capacity: 21,000 Pounds ( L) Powerplant: 3 Honeywell TFE C, 5,000 lbs each AIRFRAME Year of manufacture: 2000 Year of delivery: 2000 Year of interior refurbishment: 2012 Year of exterior repaint: 2016 Total time airframe: Hours Total landings: EU-OPS Public Transport certified Certified for 14 passengers Cargo Space 127 cu ft (3,6 m3 ) Inspections 1C/2C CW 04/2012 1A/1A+ due 08/2016 No damage history Airframe (avionics) program Honeywell HAPP and Collins CASP ENGINES Manufacturer: Mfg Part No. Engine #1 Total Time: Engine #2 Total Time: Engine #3 Total Time: Honeywell TFE C Hours Hours Hours ISSUE Page 3

4 ENGINES continued Engine #1 Total Cycles: Engine #2 Total Cycles: Engine #3 Total Cycles: Thrust Rating: Engine Program: Landings Landings Landings 5,000 Lbf JSSI APU Manufacturer: Mfg Part No. Time since new : APU Program : Honeywell GTCP (F) Hours JSSI ISSUE Page 4

5 INTERIOR This aircraft is configured for fourteen passengers. The cabin features a forward four place club, mid four place conference opposite credenza and aft dual three place berthable divans. A forward galley is equipped with Turmix C420 Automatic Nespresso machine, microwave and convection oven. Crew lavatory located in the forward cabin and fully enclosed passenger lavatory is located in the aft. All seats are light beige leather, divan is light taupe and wood finished in Bird s Eye maple wood. Interior refurbished in 2012, including new perforated leather seats (Falcon 7X sized), new carpets, new sidewall covering, and veneer varnish rework. DAY CONFIGURATION (Sample) NIGHT CONFIGURATION (Sample) ENTERTAINMENT & CONNECTIVITY Entertainment system w/12 disk CD player DVD multi-standard player Two 17 LCD monitors Four 10.7 moveable monitors Airshow 400 Auxiliary 220V ISSUE Page 5

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8 AVIONICS Honeywell Primus 2000 (5-tube EFIS) Triple Honeywell FMZ-2000 soft-5.2a Dual Honeywell Positioning System Sensors Triple Honeywell IRS Laseref III Heads Up Guidance System Triple Collins VHF-422C Dual Collins VIR-432 VHF Nav Dual Collins ADF-462 Dual Collins DME-442 Dual Collins TDR 94D Mode S Transponder w/flight ID Dual Honeywell Primus-880 Weather Radar TCAS 7.1 Collins TTR Dual Honeywell RT-300 Radar Altimeter Dual Collins HF-9034 w/avtech Selcal Honeywell AFIS Honeywell MCS-6000 Satcom Allied Signal Mark V EGPWS Allied Signal CVR (120 min) Allied Signal DFDR (32 parameters-25 hours) ELT 96 Socata (3 frequency) ISSUE Page 8

9 CONTACT ENGEL&VÖLKERS AVIATION Eric PAUWELS DISCLAIMER This offering is subject, but not limited to, errors, omissions, price fluctuation, and prior sale or withdrawal without notice. All details disclosed are without guarantee and solely based on the information received by Engel & Völkers Aviation. Engel & Völkers Aviation cannot be held liable for any lack of completeness, inaccuracy, or ambiguities and/or errors contained in the information disclosed. It is the buyer s responsibility to disclose the details of any concern(s) to the seller, by the request of an independent survey, pre-purchase inspection and/or enquiry. The buyer must ensure that the purchase contract properly reflects his concern(s) and that it sets out any representations and/or details on upon which he may rely. We are at your disposal for any further information about the aircraft. Upon receipt of notice, the aircraft is available for viewing at timing to be agreed upon, accompanied by an Engel & Völkers Aviation representative. ISSUE Page 9