The prototype Viscount V.630 first flew in 1948 and
was a short range 32 seat airliner powered by 2x 990shp (738kW)
Rolls-Royces. Airlines expressed no interest in an aircraft with this
capacity and Vickers redesigned the V.630 as the 60 seat V.700 which had
a length of 81’9"(24.91m), and was first flown in 1950 powered by 2x
1400shp(1044kW) Rolls-Royces. BEA ordered 26 examples of the V.700 and
when it entered revenue- earning service in 1953 on the BEA schedule
from London to Nicosia, it became the first turboprop airliner in the
world to enter service. The V.700D introduced the higher powered 1600shp
engines. 289 examples of the V.700 series were eventually built. The
V.800 was a stretched version. The final version of the Viscount was the
V.810 (86 built) which was first flown in 1957 powered by 2x
1800shp(1342kW) Rolls-Royces and with a maximum take-off weight of
72,500lb(32,915kg). This had a strengthened fuselage and a cruising
speed of 360mph(579kmh). A handful of Viscounts remain airworthy, with
all of those operating in Africa.
G-AZLP
c/n 346
United Kingdom
70 seat airliner first flown in 1956
Engines: 2x 1600shp(1193kW) Rolls-Royce Dart 510
Length: 85’0"(25.9m)
Height: 27’9"(8.45m)Wingspan: 93’8.5"(28.56m)
No.built: 67 Range: 1035miles(1665km)
Cruising speed: 314mph(503kmh) Empty weight: 40,200lb(18,250kg)
Maximum take-off weight: 63,000lb(28,602kg) |