Lockheed L-1011 TriStar
Lockheed L-1011 TriStar – This wide-bodied trivet was initially launched in 1968 with many orders. A strong part of the Lockheed L-1011 TriStars appeal being the new Rolls-Royce RB.211 engine. But the first RB.211 was a disaster, bankrupting Rolls-Royce in 1971 and throwing the L-1011 programmed into jeopardy. Eventually it went ahead, with excellent 42,000-lb thrust RB.211-22B engines, but the delay was serious. Even more crippling was the fact that struggling Rolls-Royce was in no position to compete with North American firms in offering engines in the over-50,000-lb class and this put the rival DC-10 airliner in a commanding position. Lockheed were able to sell only 249 official versions.
Later a more powerful R13.211 appeared and built longer-ranged L-1011s, culminating in the Series 500 with extended wings, shorter body and a range of up to 7,300 miles.
The Lockheed L-1011 TriStar can be distinguished from the DC-10 because its centre engine is inside the rear fuselage.
Like the rival L-1011, the DC-10 was planned to meet a 1966 specification set by American Airlines, which placed the launch order in early 1968. The first DC-10-10 was designed for coast-to-coast range (across the United States), carrying up to 380 passengers and powered by three 40, 000-lb thrust General Electric CF6-Engines in a novel arrangement —two under the sharply sweptback wings and one completely above the rear fuselage with the vertical tail above it. In 1972 it was joined by the DC-10-30, with an increased wingspan (from 155 ft to 165 ft), much greater fuel capacity, and an extra twin-wheelman gear on the centerline and CF6-50 engines in the 50,000-lb class.
The first DC-10s weighed 386,500 blooded, whereas later DC-10-30s weigh up to 572,000 lb and can carry a max-imam payload for 4,600 miles. The lastDC-10s of all are the DC-10-30ER (Extended Range) version, with54; 000-lb thrust engines and extra fuel for ranges up to 6,600 miles. There are large windshields and side-panel windows give good flight deck visibility. Each pilot can see 62 up and 22.5 down, and rearward vision through 135 gives a sideways view as far as the wingtips.
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