Light Jets

GULFSTREAM G-200



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AIRCRAFT DESCRIPTION

The Gulfstream 200 was one of the first private jets in the Gulfstream series, jets that would become top competitors in the super-midsize category. The newly-formed Galaxy Aerospace Corp, a division of Israel Aviation Industries (IAI), became a major contender in the private jet category with the Gulfstream 200; this jet continues to compete today with the more recent G450 and G550. The Gulfstream 200 has everything that could be desired in a private jet: great range, cabin size, and speed. It’s the ideal jet for completing long-range missions rapidly and comfortably.

The cabin of the Gulfstream 200 can be configured to hold anywhere between eight and nineteen seats. The cabin itself is 24.4 feet long, 7.2 feet wide, and 6.3 feet high. Optional additions include a radio phone, entertainment systems, and interior design upgrades. There are power outlets available for any piece of office equipment in addition to an outlet for each passenger. There is 125 cubic feet of baggage space available in an external compartment, able to contain up to 2,400 pounds.

An added bonus of the Gulfstream 200, having been designed in the extreme temperatures of Israel, is its capacity to maintain a cool cabin. According to Galaxy Aircraft Corp, the Gulfstream 200 can cool the cabin to 75ºF on a 113ºF day. Both the cabin and the cockpit have separate climate controls, and the air in the temperature control system continually provides the passengers with fresh air instead of recirculated air.

The Gulfstream 200 can climb directly to an altitude of 37,000 feet in nineteen minutes. For a long range cruise, it travels at 430 knots at an altitude of 41,000 feet; for a high speed cruise, it travels at 470 knots (.82 Mach) at 39,000 feet. The cabin is rated to 8.9 psi, meaning it can maintain a sea level cabin at 23,000 feet, or an 8,000 foot cabin at its maximum flight level of 45,000 feet. With a range of 3,910 miles (3,400 nautical miles), the Gulfstream 200 is ideal for long-range transcontinental or transoceanic missions. The required runway distance for takeoff at sea level is 6,083 feet with standard loading, or 6,342 feet when loaded to its maximum takeoff weight (MTOW) of 35,450 pounds. At an altitude of 5,000 feet and a temperature of 77ºF, the takeoff distance increases to 9,800 feet.


AIRCRAFT CHARACTERISTICS & SPECIFICATIONS(CJ2)


 

Engine
2 X Pratt and Whitney 306A
Power
6,040.00 lbf
Max Cruise Speed
850.00 km per hr 528.19 mph
Service Ceiling
13,716.00 metres  45,000.00 feets
Rate of Climb
609.60 mpm   2,000.00 fpm
Cabin Height

1.91 metres  6.27 feets

Cabin Width
2.18 metres  7.15 feets
Cabin Length
7.44 metres  24.41 feets
Exterior Length
18.97 metres  62.24 feets
Wingspan

17.70 metres  58.07 feets

Baggage Volume
150.00 cubic feet
Max Take Off Weight
16,080.12 kgs  35,450.00 lbs
Maximum Payload
1,837.08 kgs  4,050.00 lbs
Fuel Tank Capacity
2,239.00 gallon  8,475.51 litres
Fuel Economy
0.65 kmpl  1.52 NM per gallon
Min Take Off Distance
1,854.10 metres  6,083.00 feets
Min Landing Distance
999.74 metres  3,280.00 feets
Seating Chart /Seats
10
Travel Range
3,400.00 Nm - 6,297 Km
Country of Manufacture
United States

 

AIRCRAFT AVERAGE PRICE USED/NEW - ( 55crore to 150+ crore)

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