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The Airbus Helicopters H225 (formerly Eurocopter EC225 Super Puma) is a long-range passenger transport helicopter developed by Eurocopter as the next generation of the civilian Super Puma family. It is a twin-engined aircraft and can carry up to 24 passengers along with two crew and a cabin attendant, dependent on customer configuration.
By 1980, the AS 332 Super Puma had replaced the preceding SA 330 Puma as Aérospatiale's principal utility helicopter. [10] It quickly proved to be highly popular amongst its customers; between July 1981 and April 1987, on average, three helicopters per month were being built for operators from both the military and civilian sectors. [11]
The AS532 is a development and upgrade of the Aérospatiale SA 330 Puma in its militarized form. Its civilian counterpart is the Eurocopter AS332 Super Puma (Later called the Airbus Helicopters H215, note the lack of M suffix). The AS532 has been further developed as the Eurocopter EC725.
Eurocopter AS332 Super Puma The KAI KUH-1 Surion is a twin-engine, transport utility helicopter developed primarily by Korea Aerospace Industries (KAI), Agency for Defense Development (ADD) and Korea Aerospace Research Institute (KARI) jointly with Eurocopter .
Eurocopter EC225 Super Puma: ... seeking 123 helicopters to replace its aging Westland Sea King fleet. ... Rate of climb: 7.4 m/s (1,460 ft/min) See also
The Sikorsky S-92 is an American twin-engine medium-lift helicopter built by Sikorsky Aircraft for the civil and military helicopter markets. The S-92 was developed from the Sikorsky S-70 helicopter and has similar parts such as flight control and rotor systems.
In 1974, Aerospatiale began development of improved Puma variants, aiming to produce a successor to the type; these efforts would cumulate in the AS332 Super Puma. The first prototype AS332 Super Puma took flight on 13 September 1978, featuring more powerful engines and a more aerodynamically efficient extended fuselage; by 1980, production of ...
Data from International Directiory of Civil Aircraft General characteristics Crew: 2 Capacity: up to 30 passengers Length: 58 ft 11 in (17.96 m) Height: 17 ft 6 in (5.33 m) Empty weight: 12,336 lb (5,596 kg) Gross weight: 16,164 lb (7,332 kg) Max takeoff weight: 19,000 lb (8,618 kg) Powerplant: 2 × General Electric CT58-140 turboshaft engines, 1,500 shp (1,100 kW) each Main rotor diameter: 62 ...