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Gulfstream G650 for sale

Gulfstream G650 for sale information

Range (NM) 7,130
Seating 18/21
Max Speed (Kts) 516
Cruise Speed (Kts) N/A
Rate of Climb (Ft/min) 3,570
Balanced Field Length/
Landing Distance 6,285/2,665
Cabin Volume (CuFt) 2421 cu. ft.
Payload (Maximum) 6,500
Baggage (CuFt Int/Ext) 195/-
Service Ceiling (Ft) 51,000
DOC $4,210/Hour, $9.70/NM
Years of Manufacture 2012-present
Number in Fleet 60+
Estimated Market Value $69,000,000 – $73,000,000

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Gulfstream G650 for sale

Year • 2017

TTAF 0

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Price on request

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More about Gulfstream G650 for sale

Gulfstream G650 — the first airplane with big salon developed by Gulfstream Aerospace from a blank sheet since a debut of Gulfstream II which has taken place in 1967. It is no wonder that expectations of the public have been warmed very up and the developer has been actually forced to set to himself the most ambitious design tasks to supply not only a new leader, but also his possible future derivatives with the unique characteristics surpassing all previous big Gulfstream.

Finally, competitors in the person of Bombardier and Dassault do not doze at all and to contend with their latest developments far more difficult, than at the time of Gulfstream II. Gulfstream 650 – the latest business Jett applying for hegemony in the class in the nearest future. Distinctive feature is broad use of composite materials. Recently by this plane the new absolute record of speed for planes of business aircraft was set. The management of General Dynamics, the parent company Gulfstream, is sure that business jets with big salons and range not bad will be on sale soon therefore the Gulfstream G650 program has given start to strategy of powerful investment into development of new products. Allegedly, Gulfstream G650 will become basic model on the basis of which derivative models with smaller and bigger range, and also, perhaps, different length will be developed. At least it will help the American company to offer the worthy answer of Dassault and Bombardier.

Development of programs from a blank sheet — only one of new trends in Gulfstream. The company also invests heavily in modernization of productions with the purpose to cut by half quantities of details of Gulfstream G650 with the corresponding reduction of labor costs on assembly. Level of the technological innovations applied in development of Gulfstream G650, a cut above all earlier Gulfstream in the new programs was solved on. It is not always obvious, but the more you understands details, the more you can evaluate extent of their study. FEATURES OF THE DESIGN OF THE GLIDER AND SYSTEMS Basic requirements to the Gulfstream G650 program are dictated by the existing clients of Gulfstream.

In particular, they have spoken entirely in favor of careful approach to experimenting with new technologies, especially using composition materials in a glider design. So the fuselage and a wing of Gulfstream G650 are made of aluminum alloys using steel and titanium as well as in the previous Gulfstream models. Nevertheless broader application, than earlier, including in a design of stabilizers, elevation rudders and the direction, a floor of salon, a back germoshpangout, motor-gondolas, tips of a wing and a different fairing was found for composites. Elements of a power set are located with an interval of 45 cm that is less than on other Gulfstream models. First, it allows to increase distance between illuminators, so and to provide more place for legs of the sitting passengers as chairs are established concerning illuminators.

Secondly, it allows to increase illuminators that visually emphasizes roominess of salon. Engineers managed to achieve higher performance of a design and though in lateral section of Gulfstream G650 it is more, than G550, but a unit load per acre same, besides extent of sealing at it is higher. The weight of the empty airplane has increased more than by 2260 kg in comparison with the previous model owing to lengthening of a fuselage on meter, a wing of the bigger area, heavier engines and tail plumage etc. From the point of view of aerodynamics of Gulfstream G650 is the breakthrough which has left the previous “widebody” Gulfstream far behind. Designers have especially worked at a shape of a nose to reduce wave resistance and at the same time to increase the area of a glazing of a cabin and to provide to crew the best review. As before, engineers of Gulfstream have refused the rejected flaps as they believe that the additional weight and complexity of a design do not come true advantages of increase in lifting force at big angles of attack. They have made the decision in favor of a wing of 12 sq.m with the lowest indicator of a unit load among all “ultradistant” airplanes of a corporate class.

As a result take-off and landing speeds have turned out is acceptable low. Arrow-shapedness 33 ° on a quarter of a chord is urged to reduce the induced resistance, the big interfaced tips (vingleta) — to reduce failure of a flow on wing tips that is important, considering modest relative lengthening of a wing — 7,73:1,00. Thus, bearing surfaces are optimized for the cruiser speed 0,855M that is 0,055M higher, than at G550, and create 8% more lifting force. Gulfstream G650 also became the first of big Gulfstream which tailpiece of a fuselage is developed using an area rule for decrease in the interferential resistance arising between motor-gondolas and a fuselage. It is necessary to tell that Bombardier and Dassault use this method for a long time. Finally we receive the airplane with range of 7000 nautical miles (nearly 13 thousand km) at a cruiser speed higher than 0,85M or 6000 nautical miles at a speed of 0,90M. Fuel usage at a speed of 0,85M is lower, than at other representatives of the class large-cabin who are nowadays exploited. With such speed it is possible to fly without refueling from San Diego to Sydney, from Chicago to Cape Town and even from Hamburg to Hawaii.

Moreover, G650 — the first “thoroughbred” business jet (VIP-versions of airliners are not counted), which is capable to make the nonstop run New York — Tokyo (Seoul, Beijing) under not ideal atmospheric conditions and even not on the most optimum trasses. The new leader has inherited the majority of systems from G550, however they have been reviewed and modernized for the purpose of increase of extent of reservation, reliability and simplicity. For example, reservation of the electrical system is increased several times as that is demanded by EDSU and a reserve hydraulic system of flight control which also eats from the electrical system. It is remarkable that it was initially planned to use for Gulfstream G650 lithium-ion accumulators, however at the end of 2011 engineers of Gulfstream have refused this idea as the tested accumulators have not shown required results. Nickel cadmium batteries add about 70 kg to airplane weight, but they it is more reliable.

For Gulfstream G650 have designed five-channel EDSU with two main and reserve computers. Thus, the new leader became the first representative of Gulfstream with a full-fledged electroremote control system that has demanded to increase many times extent of reservation of the electrical system and to bring the number of power supplies to ten. Traditional steering wheels and pedals (production Rockwell Collins) are equipped with the converters transmitting signals on five channels to computers of flight control (FCC) and a spare block (productions Thales Canada), each of which has access to blocks of the drives (production Parker Aerospace) changing the provision of all managing surfaces.

At each FCC one channel active, the second is intended for monitoring as though two airplanes flew a dense system and in everyone one pilot was engaged in piloting, and the second — monitoring. Thus, four channels — as four pilots: all different, but have to coordinate each action. The spare block enters game only if two main computers have completely failed. Basic modes of management too four, three of them are carried out by FCC. The normal mode which uses air and inertial data in addition to teams of the pilot provides protection against an exit for borders of the admissible modes of flight, decrease in an overload at maneuver and stability increase, including on speed. There is a function of automatic compensation of the moment of pitch at change of position of flaps, air brakes and landing gear extension.

The mode works at take off and landing as direct (direct). Then the normal mode joins, but the pilot can trim manually pitch at change of speed. The similar principles are underlain in EDSU of the Boeing 777, 787 airplanes and Embraer E-Jet family. Certain failures of sensors can lead to the fact that FCC pass into the duplicative mode. In it functions of an auto pilot and protection against an exit out of limits of the normal modes of flight are turned off. Further, if the number of refusals interferes with functioning of the duplicative mode, FCC replaces the mode on a straight line, at the same time all highest functions of management, including automatic operation of air brakes and interceptors are lost. That is impacts of the pilot on governing bodies are directly transferred to drives of managing surfaces. At last, if both computers absolutely fail, the spare block which is providing all basic functions of management, but not providing the highest functions is connected.

The hydraulic system of Gulfstream G650 is almost entirely inherited at predecessors in spite of the fact that EDSU excludes need of mechanical drives. Innovative approach of Gulfstream is that seven of 16 steering linkages are hybrid, that is can function as normal electrohydraulic or as electric, from a source of a direct current, in case of refusal hydraulics. Gulfstream calls these systems reserve hydrostatic drives. Thus, sufficient reservation is provided, but need of the third, reserve, hydraulic systems is excluded. Precedent of certification of the similar scheme already is, it is used on Airbus A380, but there the electrohydraulic system of drives works as the main, but not as reserve. The Gulfstream G650 salon is 35 cm wider, 8 cm higher and is much longer, than at G550. Everything, taking into account an interior, 250 cm in width, 192 cm in height and 13 m from the partition separating a crew cabin from salon to a wall of a luggage compartment in a tailpiece turn out. From records in parameters — the widest floor from all business jets (apart from the VIP-version of regional airplanes and airliners).

In lateral section the fuselage represents not a circle, and more likely a wide oval that provides more space at the level of shoulders and elbows. The volume of salon is at 28% more, than at the predecessor, the area of a floor — for 30%. Branded unsurpassed wide oval illuminators number 16 steels 16% more so now they with a huge separation receive an honorary title of the widest illuminators in the world of business jets. At the same time fuselage design weight practically same, as at G550: impressive structural efficiency, considering that extent of sealing of salon at Gulfstream G650 is higher, than at any other “ultradistant” airplane. One more innovation for airplanes of such class — the electric drive of opening of a door. The entrance door the sizes of 192 x 90 cm is equipped with a ladder with illumination of steps and a steady handrail on both sides. Control of a door can be exercised from a workplace of cabin crew. Only technicians will be able to open a door manually during basic maintenance. Designers have developed dozen of ready options of an interior for Gulfstream G650. In the airplane which has got to us for testing the configuration of salon is called Universal 13. In it the front part of salon is given to crew (the vacation spot, a toilet and the kitchen block), the passenger cab is divided into three zones, and in a tailpiece the toilet and a luggage compartment available from salon are located. The inner trim is faultless — it is typical for Gulfstream.

The space for rest of crew (2 m in length) is separated from passenger part of salon by a strong noise-absorbing door. Here the chair 60 cm wide which is displayed in completely horizontal position (that it could be used as the certified vacation spot, it is necessary to get JetBed mattress), and a folding table is located. The simple furniture supplements the 17-inch screen on a front partition. Clothes and toilet (the benefit that there is an illuminator, a mirror and boxes for different personal belongings is transformed to an occasional seat of rest for crew members) are located behind an entrance door at once. Further the kitchen block (1,35 m) divided into the left and right half follows, each of which also has own illuminator.

On the left side — the working area with a sliding surface and a sink with the filter for water. Here microwave and convection furnaces, tanks for drinks, lockers for ware, trash bins and dirty ware are located. The right half is equipped by holders for ten bottles and glasses, boxes for ice. Here the refrigerator is placed. The sliding screen separates kitchen from the rest area of crew. The configuration of a passenger cab in general is similar to G550 configuration, but each zone is more on all measurements. On two illuminators from each party are equipped with blinds with electric management. That it is more interesting: electric management of two chairs from four in club section includes heating, regulates a deviation angle of a back and even includes massage (each chair with such management adds 13 kg to airplane weight in comparison with normal). Also, that is one pressing of the button, displays tables.

Couples of chairs located the person to each other are displayed in a bed. In addition to the general 26-inch screen which is built in in a partition as an option 12,1 inches, individual with diagonal, are offered. In the central zone “conference” the section on the left side (if necessary turns into a double bed) with sliding tables is added with a long low dresser with office equipment on right. Chairs move on 20 cm back and forth and on 13 cm to pass. The emergency exits which are also placed in the central zone (over a wing), it is twice more by the size, than in G550. In the third zone on the right board the triple sofa, behind it — a bedside table and the first-aid kit is located. On the left board — two chairs which are converted into a bed. Thus, during night run onboard G650 with comfort six passengers will accommodate. This zone it is possible at desire to isolate partitions. The toilet (1,2 m in length) is located in the tail, and in its wall there is a door in a luggage compartment, access to which in flight is limited to FL400 echelon (that is actually on a set and decrease).

Air temperature in salon is regulated separately in three zones. On FL410 echelon pressure in salon is supported at the level of 915 m above sea level, on FL510 — 1,5 thousand m. IN FLIGHT In a cabin of Gulfstream G650 (serial number 6013) to the right of me the test pilot Jake Howard, behind on folding — the test pilot Tom Horn who is carrying out functions duplicative. The weight of our airplane without fuel (and without passengers) — 24,5 t so potentially we could, having filled full tanks, to take 650 kg of payload. The empty equipped weight quite corresponds to statements of Gulfstream. According to reports of still few operators, the airplane filled to the full by the option equipment, equipped for transatlantic trip with provisions weighs from 24,67 to 24,91 t. Thus, with full gas station it can take aboard from four to seven passengers. However, each following passenger will “cost” only 35 nautical miles of range. The most part of operational documentation of Gulfstream G650 is copied from G550. Developers hoped that they will manage to distribute the admission to the G550 type and to G650. However FAA and EASA have opposed this idea because by more fixed consideration — to take from these airplanes of not so much general at least EDSU. As it was already noted, the review from a cabin has significantly improved thanks to wider glazing. Increase of situational awareness is promoted also by the system of synthetic vision (EVS) which is turning on the collimator display on a windshield (HUD).

There were onboard slightly more than 7 t of fuel, but it is enough to fly by from the Savanna (piece Georgia on east coast of the USA) 3840 km to San Diego in California at a speed of 0,85M. By Horn’s calculations, the parking weight of the airplane makes 31760 kg, that is about 70% of the maximum take-off now. An eminence of the airport of the Savanna — 50 feet above sea level. Behind a board of +25 °C. On the basis of these data we calculate: unstick speed — 109 nodes, a running start distance — 1036 m. Start of Rolls-Royce BR725 engines is carried out as well as on G550. We turn on the sucking pumps, we turn start master and we press the start button. We open the fuel crane. The rest does FADEC. I notice that for the period of start THU is disconnected, after start automatically joins. Having executed the check sheets, we begin taxing to the runway 19.

Gulfstream G650 prices:

Gulfstream G650 for sale – 62 000000 dollars US;

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Summary
Aggregate Rating
5 based on 2 votes
Brand Name
Gulfstream
Product Name
Gulfstream G650 for sale

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