WESTLAND GAZELLE Civil Aircraft Model Details

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General Information of WESTLAND GAZELLE

Developed From : Aerospatiale Alouette III

First Flight : 7 April 1967 (SA.340)

Introduction : 1973

Manufacturer : Sud Aviation; Aerospatiale

Number Built : 1775

Primary Users : French Army; British Army; Serbian Air Force; Egyptian Air Force; Lebanese Air Force

Produced : 1967-1996

Role : Utility helicopter / Armed helicopter

Status : In service

Unit_Cost : $198,500 (1973)[1]

General characteristics of WESTLAND GAZELLE

Capacity : 3 Passengers

Crew : 2

Empty Weight : 908 kg (2,002 lb)

Gross Weight : 1,800 kg (3,970 lb)

Height : 3.15 m (10 ft 3 in)

Length : 11.97 m (39 ft 0 in)

Main Rotor Area : 86.5 m2 (931 ft2)

Main Rotor Diameter : 10.5 m (34 ft 6 in)

Powerplant : 1 × Turbomeca Astazou IIIA turboshaft, 440 kW (590 hp)

Performance of WESTLAND GAZELLE

Cruise Speed : 264 km/h (164 mph)

Maximum Speed : 310 km/h (193 mph)

Range : 670 km (416 miles)

Rate Of Climb : 9 m/s (1,770 ft/min)

Service Ceiling : 5,000 m (16,405 ft)

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