WESTLAND IV Civil Aircraft Model Details

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General Information of WESTLAND IV

Designer : Arthur Davenport, Robert Bruce[1]

First Flight : 10646

Manufacturer : Westland Aircraft

National Origin : United Kingdom

Number Built : 10

Primary Users : Sabena

Role : Light Transport Aircraft

General characteristics of WESTLAND IV

Capacity : Six passengers [3]

Crew : Two

Empty Weight : 3,891 lb (1,769 kg)

Height : 9 ft 6 in (2.89 m)

Length : 38 ft 0 in (11.59 m)

Loaded_Weight : 6,300 lb (2,864 kg)

Powerplant : 3 × Armstrong Siddeley Genet Major 1A 7-cylinder air cooled radial engine, 140 hp (104 kW) each

Wing Area : 490 ft² (45.5 m²)

Wingspan : 57 ft 6 in (17.53 m)

Performance of WESTLAND IV

Cruise Speed : 100 mph (87 knots, 161 km/h)

Maximum Speed : 122 mph (106 knots, 196 km/h)

Power/Mass : 0.067 hp/lb (0.11 kW/kg)

Range : 420 mi (365 NM, 676 km)

Rate Of Climb : 680 ft/min (3.46 m/s)

Service Ceiling : 14,900 ft (4,540 m)

Wing Loading : 12.9 lb/ft² (62.9 kg/m²)

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