Falcon 2000

Falcon 2000

Features

Aircraft Type: Heavy Jet
Seat: 10 Seater
Luggage: 15 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
In-flight Audio Player: Yes
In-flight Video Player: Yes
Communication: Yes
Runway Requirement: 5,500 Feet
Range: 3,000 NM
Cabin Height: 6.2 Feet

Description

Eight years after the release of the successful Falcon 2000, Dassault released the Falcon 2000EX. It still had all of the components that made the Falcon 2000 great economy, speed, a large cabin but improved on all of these elements to make an even better jet. The cabin of the Dassault Falcon 2000EX has a volume of more than 1,000 cubic feet and usually seats between eight and twelve passengers. A seating arrangement for as many as 19 passengers can be configured, if necessary. In the standard eight-to-twelve seating arrangement, two seats can stretch out flat and combine so that passengers can actually lay down for a nap, just as they would do in a bed. True to the French dedication to style, a wide variety of interior decorating options are available for example, there are eighteen different metal finishes to choose from just for the bathroom sink alone. 131 cubic feet of baggage space is available, a total of 1,600 pounds.

Embraer ERJ 135

Embraer ERJ 135

Features

Aircraft Type: Heavy Jet
Seat: 37 Seater
Luggage: 50 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
In-flight Audio Player: Yes
In-flight Video Player: Yes
Runway Requirement: 6,000 Feet
Range: 1,750 NM
Cabin Height: 5.8 Feet

Description

The Embraer Legacy Shuttle began life as a highly successful commercial aircraft in 1999. Its parent company, Embraer, decided that their popular 50-passenger commercial jet, the ERJ-135, would translate well into a 13-passenger private jet. The resulting aircraft was a cross between the ERJ-135 and -145, and was met with success in the private jet industry. Modified in several ways to meet the needs of corporate jet flyers, the jet retained a large majority of its original design. Although the EMB-135 was the first of the Embraer private jets, it already boasted plenty of experience in the field. The most notable modifications made to the EMB-135 were the addition of winglets (increasing speed and stability), and the addition of several auxiliary fuel tanks (increasing the jet’s fuel capacity from 11,300 pounds to 18,160 pounds). Two years later, Embraer released the EMB-135LR, another model that has fared well since its debut in 2004. The EMB-135LR, in contrast to its predecessor, is designed to work best on shorter trips. It can carry more passengers than its predecessor, and is designed to be used as a corporate shuttle for anywhere between 16 and 37 passengers, not as a luxurious office at 39,000 feet.

Citation XLS

Aerial photography of the Textron Cessna Citation XLS+ jet. The XLS+ is the best selling business jet in the world; with transcontinental range this midsize jet can seat up to 12 passengers.

Pikes Peak Region
Colorado Springs, CO  USA

Features

Aircraft Type: Medium Jet
Seat: 8 Seater
Luggage: 15 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Runway Requirement: 4,000 Feet
Range: 1,850 NM
Cabin Height: 5.6 Feet

Description

The Citation XLS is technically a mid-sized jet its cabin length is 18.7 feet and it can fly up to 1,961 miles (1,704 nautical miles); however, it can also take off in 3,500 feet and climb to cruise altitude in just 18 minutes, performance statistics reminiscent of light private jets. At any rate, the XLS boasts excellent handling capabilities, reliable systems, and consistent delivery of smooth, quick flights. The XLS is the updated version of the Citation Excel and goes faster and further than its predecessor. The 5.7 feet high interior of the XLS holds nine passengers in a cabin thats quiet and draft-free, due to the triple-sealed entry door and triple-pane windows. Details like fold-out tables, sliding headrests, and seats two to four inches wider than in previous models make flying comfortable. A couch (rated to take off /landing safety standards) comes standard. Indirect LED lighting is installed to give the cabin a roomier, more natural feel and comes with the benefits of producing less heat and lasting longer. An external compartment provides 80 cubic feet of storage space, along with some additional space in an internal closet. This private jet can climb to its flight level of 43,000 feet in just twenty five minutes (48 minutes faster than the Excel) and can cruise at 428 ktas. The XLS can reach a range of 1,941 miles (1,687 nautical miles) with four passengers. It can take off on runways as short as 3,500 feet the shortest take off distance of any midsized jet.

Challenger 605

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Features

Aircraft Type: Heavy Jet
Seat: 8 Seater
Luggage: 16 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
In-flight Audio Player: Yes
In-flight Video Player: Yes
Communication: Yes
Runway Requirement: 5,500 Feet
Range: 4,000 NM
Cabin Height: 6.2 Feet

Description

Bombardier’s Challenger series, perhaps its most successful line, has only become better with experience.Because the original Challenger was so successful, Bombardier continues to use its general design while incorporating up-to-date technology and improvements on well-received components. It would be a challenge, pun intended, to fill the shoes of the Challenger 604, the best-selling model in the heavy-iron category. However, the Challenger 605 maintains every praised feature of its predecessor, adding freedom, innovation and performance capabilities. It’s no wonder that this $27 million long-range business jet is a valuable asset to corporate clients.For good reason, Bombardier chose to preserve the spacious Challenger cabin that has accommodated business travelers for years. In a combination of club, divan and individual seating, the Challenger 605 typically carries 10-12 passengers. Cabin measurements are 6.1 feet tall, over 7 feet wide and 28.3 feet long, almost necessary for long-duration flights. However, it has been completely restyled to reflect customers every desire. Larger and higher-positioned windows make for ideal viewing pleasure. It has an improved Ethernet-based management system, larger video monitors, an upgraded galley area, sturdier worktables and more LED lighting. Overall, the Challenger 605’s cabin offers more in every respect.

Challenger 604

challenger 605 EXT

Features

Aircraft Type: Heavy Jet
Seat: 10 Seater
Luggage: 16 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
In-flight Audio Player: Yes
In-flight Video Player: Yes
Communication: Yes
Runway Requirement: 5,500 Feet
Range: 4,000 NM
Cabin Height: 6.2 Feet

Description

Beginning with the original Challenger 600, Bombardier created a successful family of business jets. After numerous refinements and upgrades, the Challenger 604 secures the family name in the long-range, business jet market. Certified in 1995, the 604 provides range, speed, and sophistication and style.A lot of power can be found in the Challenger 604. Two General Electric CF34-3B engines propel the jet, each rated at 8,729 lbs of thrust. This means that with eight passengers, the 604 can fly 3,850 miles, and at .74 Mach. However, 4,000+ nautical mile legs are possible at 424 ktas (a personal milestone for Canadair) due to new fuel distribution and greater capacity (2,460 gallons).Like the Challenger 601-3A, the aircraft consists of a glass cockpit: the Collins Pro Line 4. Six screens (7.25 inches) show left and right primary flight displays, multifunction displays and EICAS. The avionics suite also includes pilot-friendly features such as flight director/autopilot systems, HF-9000 high frequency radios, digital air data computers, turbulence detection radar and dual Pro Line 400 all-digital interface comm/nav/ident radios. All contribute to the ease and comfort of flying.

Cessna CJ2

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Features

Aircraft Type: Light Jet
Seat: 8 Seater
Luggage: 12 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
Runway Requirement: 4,000 Feet
Range: 1,400 NM
Cabin Height: 4.7 Feet

Description

The CJ2 is quite fuel-efficient, with an average fuel burn of 140 gallons per hour. The economy of its fuel burn can be largely attributed to Cessna’s choice of engines. It uses two Williams/Rolls-Royce FJ44-2C turbofan engines, each of which delivers 2,400 lbs. of thrust on take off (400 lbs. more than the CJ1 and CJ1+).The CJ2 can take off in 3,420 feet at sea level, or in 5,080 feet on a runway at an altitude of 5,000 feet. It takes seventeen minutes to climb to 37,000 feet. At its maximum certified flight ceiling of 45,000 feet, it reaches its long range cruise speed of 352 knots. Its high speed cruise is 407 knots. All of the cabin’s pressurization systems (certified to 8.9 psi) are controlled digitally, able to maintain a sea-level cabin pressure at 23,586 feet.The CJ2 is extremely easy to fly and can be single-pilot operated. The Citation line was designed for forward-thinking businessmen that would fly their own private jets to and from business meetings, resulting in several automated systems and a simple avionics system. For those that don’t plan to fly their own jet, its ability to be flown by a single pilot offers greater flexibility in flight operations and reduced per-hour flight costs.

Avanti 180

Avanti 180

Avanti 180

Features

Aircraft Type: Turbo Prop
Seat: 6 Seater
Luggage: 8 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
Runway Requirement: 4,000 Feet
Range: 1,700 NM
Cabin Height: 4.7 Feet

Description

The Avanti’s turboprop engines are placed on a mid-set, high aspect ratio wing located just behind the cabin. The three-surface design incorporates both a T-tail and a pair of small, fixed fore wings having slight anhedral and landing flaps. On the Avanti II these flaps automatically deploy in concert with the main wing flaps. This reduces the load on the tail plane, even when the flaps are deployed, by reducing the pitch-down moment created by the deployment of the main wing flaps. This in turn allows the size of both the tail plane and the main wing to be reduced. This particular three-lifting-surface configuration was patented in 1982. The forward wing’s angle of incidence is slightly greater than that of the main wing, so that it stalls before the main wing, producing an automatic nose-down effect prior to the onset of main wing stall; its five-degree anhedral (negative dihedral) keeps the stream wash interference clear of the engine inlets, the main wing and the tail plane.