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Aerospatiale SA-330 Puma
In the early 1960’s Sud-Aviation began development of a twin-turbine all-weather tactical and logistics transport, the first of two prototypes making its first flight on 15 April 1965. The Anglo-French helicopter agreement which ended on 2 April 1968 gave the UK company Westland Helicopters joint production rights of this helicopter, named the SA 330 Puma.
The Puma’s fuselage is of a conventional all-metal semi-monocoque construction, the engines mounted on top, forward of the main rotor assembly. The main rotor is driven by a gearbox, which combines the output from the engines to the main drive shaft. The tailboom is of monocoque construction and has a five-bladed tail rotor on the starboard side and a horizontal stabilizer on the port side. The landing gear is a semi-retractable tricycle type with twin wheels on each unit.
The Puma has been used in both civilian and military roles. Its twin-engine safety also makes it ideal for offshore transports to oil rigs and ships. Some versions also have filters forward of the air intakes improving its safety in sandy conditions.
Performance
Max speed: 262km/h (141kt)
Max cruising speed at sea level: 257km/h (139kt)
Hovering ceiling in ground effect: 7315ft
Initial rate of climb: 1400ft/min
Max range with standard fuel: 550km (297nm)
Weights
Empty: 3766kg (8305lb)
Max takeoff: 7500kg (16,535lb)
With sling load, standard max takeoff weight: 7400kg (16,315lb)
Dimensions
Rotor diameter: 15.08m (49ft 6in)
Length overall: 18.15m
Fuselage length: 14.06m (46ft 2in)
Height: 5.14m (16ft 11in)
Main rotor disc area: 177.0m2 (1905sq ft)
Capacity
Crew: one or two pilots on flightdeck, plus jumpseat
Passenger configurations in main cabin: range from 8, 10 or 12 seat executive layouts, or for 17 to 20 passengers in an airline arrangement
External sling load: 3200kg (7055lb) |
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Title: Aerospatiale SA-330B Puma
Artist:
Size: 19 1/2 x 13 3/4 in (49.5 x 35 cm)
Material: watercolor, crayon, pastel on paper
Year: 2004
Price: 75.00$
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