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Sale Boeing 777-200
Year:
2004
Passengers:
440
TTAF:
50200
Location:
USA
S/N:
TBA
Price:
Make Offer

The Boeing 777-200 is a family of long-range wide-body twin-engine jet airliners developed and manufactured by Boeing Commercial Airplanes. It is the world's largest twinjet and has a typical seating capacity for 314 to 396 passengers, with a range of 5,240 to 8,555 nautical miles (9,704 to 15,844 km). Commonly referred to as the "Triple Seven", its distinguishing features include the largest-diameter turbofan engines of any aircraft, six wheels on each main landing gear, fully circular fuselage cross-section, and a blade-shaped tail cone. Developed in consultation with eight major airlines, the 777 was designed to replace older wide-body airliners and bridge the capacity difference between Boeing's 767 and 747. As Boeing's first fly-by-wire airliner, it has computer-mediated controls. It was also the first commercial aircraft to be designed entirely with computer-aided design. The 777 is produced in two fuselage lengths as of 2014. The original 777-200 variant entered commercial service in 1995, followed by the extended-range 777-200ER in 1997. The initial 777-200, -200ER and -300 versions are equipped with General Electric GE90, Pratt & Whitney PW4000, or Rolls-Royce Trent 800 engines. The extended-range 777-300ER and ultra long-range 777-200LR variants entered service in 2004 and 2006 respectively, while the 777F, a freighter version, debuted in February 2009; these variants all feature high-output GE90 engines and extended raked wingtips. The 777-200LR is the world's longest-range airliner, able to fly more than halfway around the globe, and holds the record for the longest distance flown non-stop by a commercial aircraft.

Technical information



Passenger capacity

up to 280 (3 or 4 class)

Length

63.7m (209 feet 1 inches)

Wingspan

60.9m (199 feet 11 inches)

Height

18.5m (60 feet 9 inches)

Engines

2× Rolls Royce Trent 800 or 2× General Electric 90

Maximum speed

950km/h (590mph, Mach 0.89)

Range

6,857km (4,261 miles)

 

 

 Specifications

 
  777-200ER 777-200LR

Weight
Maximum take-off weight (kg) 263 080 - 297 560 322 050 - 347 800
Maximum landing weight (kg) 208 650 - 213 190 220 900 - 223 170
Operating empty weight (kg) 135 600 - 143 800 155 580 - 156 030
Maximum zero fuel weight (kg) 195 000 - 199 580 206 840 - 209 110
Maximum payload (kg) 51 250 50 850
Standard fuel capacity (litres) 171 170 202 500
Performance
Range with max payload (km) 10 750 - 14 300 15 040 - 17 450
Cruise speed (km/h) 905 905
Maximum speed (km/h) 945 945
Maximum operating altitude (m) 13 100 13 100
Take-off field length (m) 3 000 2 900
Landing field length (m) 1 630 1 700
Engines GE GE90-94B,
2 x 93700 lb
P&W PW4090,
2 x 90100 lb
R-R Trent 895,
2 x 93250 lb
GE GE90-110B1,
2 x 110000 lb