The 777-200 is a wide-body twinjet from Boeing Commercial Airplane Group. The newest member of the Boeing family of jetliners has been "market-driven" to meet airline demand for a jetliner sized between the company's 767-300 and 747-400.
Configuration |
Passengers |
---|---|
Three class |
305 to 328 |
Two class |
375 to 400 |
All economy |
418 to 440 |
Variation in seating depends on an airline customer's choice of nine- or 10-abreast seating in economy class, and seven- or eight-abreast seating in business class.
Interior configurations: Seating ranges from six- to 10-abreast with two aisles.
Length |
209 feet 1 inch (63.7 m) |
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Wingspan |
199 feet 11 inches (60.9 m) |
Tail height |
60 feet 9 inches (18.5 m) |
Exterior fuselage diameter |
20 feet 4 inches (6.19 m) |
Interior cross-section width |
19 feet 3 inches (5.86 m) |
Cargo capacity |
Up to 32 LD-3 containers, plus 600 cubic feet (17 cubic meters) bulk-loaded cargo. Total volume 5,656 cubic feet (160.16 cubic meters). |
Number of parts: The 777-200 has about 132,500 engineered, unique parts. Including rivets, bolts and other fasteners, the airplane has more than 3 million parts.
Program launch |
Oct. 29, 1990 |
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Start major assembly |
Jan. 21, 1993 |
Ceremonial rollout |
April 9, 1994 |
First flight |
June 12, 1994 |
FAA/JAA type design and FAA production certification |
April 19, 1995 |
First delivery |
May 15, 1995 |
FAA ETOPS approval |
May 30, 1995 |
First revenue service flight |
June 7, 1995 |
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FROM: |
TO: |
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Max. takeoff weight |
506,000 pounds (229,520 kg) |
545,000 pounds (247,210 kg) |
Range |
4,210 statute miles (6,770 km) |
5,620 statute miles (9,050 km) |
Engine choices |
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Fuel capacity |
31,000 gallons (117,335 L) |
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FROM: |
TO: |
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Max. takeoff weight |
580,000 pounds (263,090 kg) |
632,500 pounds (286,900 kg) |
Range |
6,660 statute miles (10,720 km) |
8,270 statute miles (13,320 km) |
Engine choices |
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Fuel capacity |
45,220 gallons (171,160 L) |
777-200 initial model |
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777-200 increased gross weight model |
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