The British Aerospace BAE

Aircraft manufacturers had, for some 4 a long time, attempted to design the elusive DC-three replacement with different powerplant types, including the piston-engined Convair 240/340/440 and Martin 2-0-2/4-0-4 series and the turboprop Vickers Viscount, Fokker F.27 Friendship, and Hawker Siddeley HS.748. Of the 2, de Havilland, with its previous Rapide, Dove, and Heron pistonliners, had had appreciable regional aircraft experience and had designed the world's first pure-jet airliner in the form of the quad-engined DH.106 Comet. An preliminary study for such a DC-three substitute, designated the DH.123, had featured a 60.6-foot total length, an 81.3-foot wingspan, two 1,150 shp Gnone turboprops hooked up to a high wing, and a 22,100-pound maximum take off weight. 1. Suitable pure-jet engine availability.

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The bottom speed had pinnacled at 411 knots. Descent, initiated with fifty four miles remaining on its flight plan, had been attained by dialing in 5,500 toes within the cockpit's "ALT SEL" autopilot, resulting in a 2,000-fpm descent charge. Emerging from the ceiling mist over the baby blue of Lake Kariba, which had been outlined by its dry, tan and brown scrub shoreline, the captain consulted his landing flap chart corresponding to a 34,500-kilo weight.

Leaning into a proper bank over the brown and tan African expanse at 4,200 toes, the BAe-146 retracted its flaps from the 24- to the 0-degree place, finishing its "After Take Off" guidelines. Ascending by means of 7,600 toes, at which time a 291-knot floor pace had been registered, it maintained a 1,800-fpm climb rate. Its NAV indicated a 135.4-mile distance to Kariba.

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