Learjet 45

Features

Aircraft Type: Light Jet
Seat: 9 Seater
Luggage: 15 Baggage
Runway Requirement: 5,000 Feet
Range: 1,700 NM
Cabin Height: 4.7 Feet

Description

The Learjet 45 is a light jet. Designed to fly faster, higher and farther with more guests and range flexibility, this jet offers the longest cabin and more seated head, shoulder and legroom than its competitors. The Learjet 45 can fly 2,099 miles nonstop and can cruise at 465 mph. . The interior of the Learjet 45 is designed to offer the most usable passenger space possible so that the passengers do not feel claustrophobic. The Learjet 45 is an extremely reliable jet with great cruise performance and fuel economy. Its innovative systems and efficient performance make it a viable option for anyone in search of a high-performing, cost-effective private jet. Built to execute short trip and short runways, these jets are fast flying solution that offers increased access and economical benefits The Learjet 45’s cabin holds eight seats with plenty of room to swivel, recline, and track. Other fine points of the cabin’s design make it functional and comfortable, from work tables that fold down from the walls to an extra pressure relief port on the door for added passenger safety. The noise level in the cabin never exceeds 72 dB, and a two-zone temperature control system ensures that both the cabin and the cockpit are kept comfortable. An external compartment provides 50 cubic feet of baggage space with an additional 15 cubic feet of storage in the interior.

Premier 1A

Features

Aircraft Type: Light Jet
Seat: 6 Seater
Luggage: 10 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
Runway Requirement: 5,000 Feet
Range: 1,360 NM
Cabin Height: 5.3 Feet

Description

The Premier 1A’s cabin is one of the biggest for a private jet of its size, seating six or seven passengers in a 315 cubic-foot cabin. Measurements are 13.5 feet long, 5.4 feet tall and 5.5 feet wide. The cabin is designed with contoured headroom for maximum passenger comfort. Fold-out tables on both sides of the aircraft, LED lighting and fully reclineable, extra-wide, contoured seats further prove the aircraft’s comfortability. Also available are an array of cabin entertainment systems and interior trim/finish upgrades. There is 77 cubic feet of baggage space available in internal and external baggage compartments.The Premier 1A can take off in 3,792 feet and climb to 37,000 feet in seventeen minutes when loaded to its maximum takeoff capacity of 12,500 pounds. Its cruise speeds can reach 451 ktas (.80 Mach) and it can fly 1,380 nautical miles. It has a certified ceiling of 41,000 feet.

Phenom 100

Features

Aircraft Type: Light Jet
Seat: 6 Seater
Luggage: 10 Baggage
Lavatory: Yes
Runway Requirement: 4,000 Feet
Range: 1,100 NM
Cabin Height: 4.7 Feet

Description

Made by one of the largest aircraft manufacturers in the world, Brazil-based Embraer, the Phenom 100 is a very light twin engine jet. Able to accommodate four passengers and a single pilot, this small private jet is ideal for individuals or small companies.The Phenom 100 has a comfortable range of 1,160 nautical miles and can climb to 37,000 feet in just 23 minutes.The Phenom 100 is also powerful. Two Pratt and Whitney PW617F-E engines power the Phenom 100, providing a thrust for takeoff of 1,695 pounds each. These engines employ a FADEC (Full Authority Digital Electrical Control) system, making them extremely efficient and simple in flight. The engine inspection interval is 3,500 hours.It may be classified as a very light private jet, but the Phenom 100 is competitive with larger private jets in performance and space. Its high speed cruise of 380 knots true airspeed trumps all close competitors.The interior of the Phenom 100 is surprising for its size as well. Measurements are 11 ft long, 4’11” high and 5’1″ wide. The jet boasts 305 cubic feet of total cabin volume and 55 cubic feet of baggage capacity.Being a very light private jet, the Phenom 100 offers much of the same capabilities and characteristics that are specific to a class higher, but still at a fraction of the cost.

Mustang

Features

Aircraft Type: Light Jet
Seat: 4 Seater
Luggage: 4 Baggage
Runway Requirement: 3,700 Feet
Range: 1,000 NM
Cabin Height: 4.5 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.

Legacy 650

Features

Aircraft Type: Heavy Jet
Seat: 13 Seater
Luggage: 18 Baggage
Multi-course Meal on Board: Yes
Lavatory: Yes
Flight Attendant: Yes
Runway Requirement: 4,000 Feet
Range: 3,900 NM
Cabin Height: 6.1 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.

King Air C90

Features

Aircraft Type: Turbo Prop
Seat: 6 Seater
Luggage: 10 Baggage
Runway Requirement: 3,500 Feet
Range: 1,200 NM
Cabin Height: 4.7 Feet

Description

The Model C90-1 entered production in 1982 after 507 C90s and 347 E90s had been built, and featured PT6A-21 engines and improvements to the pressurization system. 54 were built. The following year the F90-1 was put into production with redesigned engine cowlings, upgraded PT6A-135A engines, hydraulic landing gear, and triple-fed electrical bus; only 33 were built by the time production terminated in 1985. The C90-1 was soon followed by the Model C90A, which featured the redesigned engine cowlings of the F90-1. The C90A received an increase in MTOW in 1987, being certified to 10,100 lb (4,580 kg). The C90A model was in production until 1992, by which time 235 had been built, all but 74 with the increased MTOW. Only two C90As were built in 1992, the Model C90B followed that year with airframe improvements, four-bladed propellers, and propeller synchrophasing, all in an effort to reduce cabin noise. This model also had PT6A-21s; the first production C90B was fitted with the 10,000th PT6 engine delivered to Beechcraft. In 1994 a cheaper version was introduced as the C90SE (Special Edition), with three-bladed propellers, standardised interior and mechanical instruments instead of the Electronic Flight Instrument System (EFIS) fitted to the C90B. A total of 456 C90Bs and C90SEs were delivered by the time production of these models ended in late 2005.

King Air B200

Features

Aircraft Type: Turbo Prop
Seat: 8 Seater
Luggage: 15 Baggage
Runway Requirement: 3,500 Feet
Range: 1,700 NM
Cabin Height: 4.7 Feet

Description

A total of 14 B200s were produced in 1989 and 1990 in a 13-seat high density configuration with a belly cargo pod; these were marketed by Beechcraft as a commuter airliner under the designation Model 1300. Customers for this version included Mesa Airlines. The propeller installation changed again in 1992, when Beechcraft started offering the option of having 4-bladed Hartzell or McCauley propellers, or 3-bladed Hartzell propellers; the 3-bladed McCauley propellers were no longer available. From October 1995 Beechcraft offered an updated B200 with Electronic Flight Instrument System (EFIS) avionics, this was marketed as the “B200SE Super King Air (for Special Edition). The following year the “Super” name was dropped from all marketing and advertising. In October 2003, Beechcraft announced another avionics upgrade for the B200, the Rockwell Collins Pro Line 21 suite. The B200 remains in production, with a total of 13 built in 2009. The B200C is available for order; in January 2009 two B200Cs were delivered to the Royal Flying Doctor Service of Australia (RFDS). The two B200Cs were the first examples delivered in about three years (the most recent B200Cs prior to this were two delivered in early 2006 for use as air ambulances in Scotland). On May 21, 2007, during the 7th Annual European Business Aviation.

Hawker 900XP

Features

Aircraft Type: Medium 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: 2,800 NM
Cabin Height: 5.6 Feet

Description

The long-range business jet features an enhanced variation of the 850XP’s winglets, increasing hot/high-altitude and cruise performance and range. On the runway in hot/high conditions, the 900XP requires 1,800 feet less runway for a 2,000 nautical mile trip with six passengers. It can complete coast-to-coast trips,With a cabin as roomy as the 850XP’s, its no wonder Raytheon chose to reuse the design for the 900XP. With a 604 cubic ft. cabin, the aircraft surpasses all others in its class. Features of the cabin include stand-up headroom, LCD lighting, touch-screen seat controls, fully-berthable seats and plenty of in-cabin storage. The cabin accommodates eight passengers.The 900XP business jet offers unbeatable fuel efficiency, performance, intuitiveness and comfort. Although improved from earlier Hawker models, the 850XP lacks the power and range of the 900XP. It is simply more machine.

Gulfstream G150

Features

Aircraft Type: Medium Jet
Seat: 7 Seater
Luggage: 12 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: 5,600 Feet
Range: 3,200 NM
Cabin Height: 5.7 Feet

Description

The Gulfstream G150 medium range, multi engine turbofan business aircraft that has an oval-shaped cabin provides ample head and shoulder room for up to eight passengers. In the cockpit, advanced flight-deck technology assures a smooth, safe ride. G150 flies at a faster cruise speed than any other midsize jet, G150 travellers will arrive more than an hour ahead of other aircraft in its class. With a maximum range of 3,000 nautical miles/5,556 kilometres at Mach 0.75, the G150 is one of the few aircraft in its class to reliably fly from California to Hawaii nonstop. It is powerful, versatile and reliable, outfitted with a variety of innovation that present you a new level of comfort and convenience The vertically elongated interior creates straighter, taller side walls, which provide more room for passenger comfort. A two-seat, side-facing divan provides greater passenger comfort than other aircraft because the straighter walls allow for more head room when seated. Shape is important in Gulfstream windows, too. In the G150, 11 large, oval windows welcome plentiful natural light and create a sense of spaciousness.

Global 6000

Features

Aircraft Type: Heavy Jet
Seat: 15 Seater
Luggage: 20 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: 6,500 Feet
Range: 6,000 NM
Cabin Height: 6.2 Feet

Description

The Global 6000 is a ultra long range jet, the Global 6000 has the largest cabin volume of any purpose-built business aircraft.The aircraft features a unique system which enables the aircraft to be refueled in less than 15 minutes, a unique feature for an aircraft of its class. Long Range Jet aircraft optimally blend comfort, performance and economy for medium length to long range flights. Cruising at speeds over 450 knots and a non-stop range of over 5000 miles, these jets travel further, faster and with more comfort than any other private jet aircraft. Its flexible wing structure affording one of the most comfortable rides in rough air compared to any purpose-built business aircraft. It has improved acoustical insulation. Cabin sound levels are among the lowest in the business aircraft industry. Bombardier’s Vision flight deck, powered by Rockwell Collins Pro Line Fusion avionics, is perhaps the biggest upgrade from the XRS to the 6000. Compared to the Honeywell Primus 2000 package installed in the original Global Express and Global XRS, the Global 6000’s Vision cockpit has provisions for current and future air traffic management requirements, including RNP approaches, controller to pilot data link communications (CPDLC), automatic dependent surveillance (ADS-B) and LPV approaches.