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Are you interested in parts and components for the HAL Chetak and similar rotorcraft? The HAL Chetak is a light utility helicopter, presently produced under licence by Hindustan Aeronautics Limited (HAL). The HAL Chetak serves as a continued production of the Aérospatiale Alouette III, designed and produced by Sud Aviation from the years between 1961 to 1985. With over 2,000 units produced as of the present, many still remain in the active service of operators such as the French Armed Forces, Indian Armed Forces, and Protuguese Air Force. Over the years of production, multiple variants of the model were released, each bringing various performance and physical changes.

Aircraft Model Hal Chetak Details

Model No : Hal Chetak
Aircraft Type : Mid Size Helicopter
Manufacturer : Hindustan Aeronautics Limited
Country : India
Manufactured : 1992 to: Present
ICAO : NA
Avionics : NA
Engine : 1 × Turbomeca Artouste IIIB turboshaft
Power : 570 horse[Power]
Max Cruise Speed : 100 knots - 185 Km/h
Approach Speed : NA
Travel Range : 292 Nautical Miles - 541 Kilometers
Fuel Economy : 2.19 nautical mile / gallon - 1.071 kilometres / litre
Service Ceiling : 17,716 feet
Rate of Climb : 950 feet/minute - 4.83metre/second
Take Off Distance : NA
Landing Distance : NA
Max Tak eOff Weight : 2,200 Kg - 4,850 lbs
Max Payload : 970 Kg - 2,138 lbs
Fuel Tank Capacity : 152 gallon - 575 litre
Baggage Volume : NA
Seats Economy/General Class : 5 seats
Seats Business Class : 0
Seats First Class : 0
Cabin Height : NA
Cabin Width : NA
Cabin Length : NA
Exterior Length : 10.03 metre - 32.91 feet
Tail Height : NA
Fuselage Diameter : NA
Wing Span Rotor Diameter : 11.02 metre - 36.15 feet
Wing Tips : NA
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For its engine configuration, the HAL Chetak features a single Turbomeca Artouste IIIB turboshaft engine that produces 570 horsepower, enabling the helicopter to reach a maximum cruise speed of 100 knots. With a fuel tank capacity of 152 gallons, the HAL Chetak may travel upwards of 292 nautical miles with an average fuel economy of 2.19 nautical miles per gallon. In general, two crew members are required for the piloting of the rotorcraft, and upwards of five passengers may be situated across available cabin seating. Accounting for cargo and passengers, the HAL Chetak operates with a maximum payload capacity of 2,138 pounds.

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