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    Malaysian PM: Flight MH370 'ended in south Indian Ocean'

    Updated: 2014-03-24 22:02 (Agencies/chinadaily.com.cn)
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    Boeing 777-200 interior seat map:

    Malaysian PM: Flight MH370 'ended in south Indian Ocean'

    Boeing's wide-body 777 was originally conceived as a stretched 767, but the company instead adopted an all new design.

    Notable 777 features include a unique fuselage cross section, Boeing's first application of fly-by-wire, an advanced technology glass flight deck with five liquid crystal displays, comparatively large scale use of composites (10 percent by weight), and advanced and extremely powerful engines.

    The 777 was also offered with optional folding wings where the outer 6m/21ft of each would fold upwards for operations at space restricted airports.

    The basic 777-200, launched in October 1990, was offered in two versions, the basic 777-200 (initially A-Market) and the increased weight, longer range 777-200IGW (Increased Gross Weight, initially B-Market). The IGW has since been redesignated 777-200ER.

    The 777-200 first flew on June 12, 1994, with Federal Aviation Administration and Joint Aviation Authorities certification awarded on April, 19 1995. The FAA awarded full 180 minutes Extended range Twin Operations clearance for PW4074 -200s on May 30 that year. The first customer delivery was to United Airlines in May 1995. The first 777-200IGW/ER was delivered to British Airways in February 1997. (airliners.net)

    777-200/777-200ER technical characteristics:

    Models 777-200 777-200ER

    Passengers

    Typical 3-class configuration

    Typical 2-class configuration

    Typical 1-class configuration

    305

    400

    up to 440

    301

    400

    up to 440

    Cargo

    Total volume 5,330 cu ft

    (151 cu m) includes up to

    six pallets, 14 LD-3

    containers, plus 600 cu ft

    (17 cu m) bulk cargo.

    same

    Engines

    maximum thrust

    Pratt & Whitney 4077

    77,000 lb

    Rolls-Royce Trent 877

    76,000 lb

    General Electric GE90-77B

    77,000 lb

    Pratt & Whitney 4090

    90,000 lb

    Rolls-Royce Trent 895

    93,400 lb

    General Electric 90-94B

    93,700 lb

    Maximum Fuel Capacity

    31,000 US gal

    (117,340 L)

    45,220 US gal

    (171,170 L)

    Maximum Takeoff Weight

    545,000 lbs

    (247,200 kg)

    656,000 lbs

    (297,550 kg)

    Maximum Range

    5,240 nautical miles

    (9,700 km)

    Typical city pairs:

    London - New York

    Denver - Honolulu

    Tokyo - San Francisco

    7,725 nautical miles

    (14,305 km)

    Typical city pairs:

    London - Los Angeles

    Tokyo - Sydney

    Chicago - Seoul

    Typical Cruise Speed

    at 35,000 feet

    0.84 Mach Same

    Basic Dimensions

    Wing Span

    Overall Length

    Tail Height

    Interior Cabin Width

    Diameter

    199 ft 11 in (60.9 m)

    209 ft 1 in (63.7 m)

    60 ft 9 in (18.5 m)

    19 ft 3 in (5.86 m)

    20 ft 4 in (6.19 m)

    199 ft 11 in (60.9 m)

    209 ft 1 in (63.7 m)

    60 ft 9 in (18.5 m)

    19 ft 3 in (5.86 m)

    20 ft 4 in (6.19 m)

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