Agusta AW119Kx

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der Frachtflug
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    The AW119Kx, an evolution of the successful A119Ke, is a spacious top of the range single turbine helicopter developed to enhanced safety levels and providing high productivity and performance at a competitive price.  A modern glass cockpit configured with Garmin’s G1000HTM  Integrated Flight Deck system enhances situational awareness. The avionic suite comprises a Synthetic Vision System with Highway In The Sky (HITS) depiction, moving map and a Helicopter Terrain Avoidance Warning System (HTAWS) with worldwide terrain and obstacle database. The large unobstructed cabin permits rapid reconfiguration for a variety of missions such as passenger transport, emergency medical service, and law enforcement applications. The versatility and high power margins of the helicopter deliver outstanding performance in a wide range of operating conditions that make it a very cost-effective helicopter. AW119Kx VIP/Corporate customers can benefit from unparalleled comfort levels among single turbine helicopters in ‘club’ seating configuration of the cabin, which is segregated from the cockpit area. A generous baggage hold in the tail section accommodates up to 150 kg of luggage. A high passenger load combined with range capability has led the helicopter to be successfully introduced into Offshore applications. The emergency medical service variant accommodates up to two stretchers and two medical attendants, in a fully medicalised cabin. When operational demands call for a single turbine powered helicopter, no other aircraft can match the cost effectiveness and superior performance of the AW119Kx.

     

    Weights

    Max take off (int. loads)

    2850

    kg

    6283

     lb

    Max take off (ext. loads)

    3150

    kg

    6945

    lb

    Basic empty weights

    1483

    kg

    3269

    lb

    Engine Rating (Pratt & Whitney PT6B-37A)

    Take off

    747

    kW

    1002

    shp

    Maximum continuous power

    650

    kW

    872

    shp

     Transmission Rating

    Take off

    684

    kW

    917

    shp

    Maximum continuous power

    671

    kW

    900

    shp

    Fuel Capacity

    3-cell fuel system

    605

    l

    160

    USgal

    4-cell fuel system

    711

    l

    188

    USgal

    5-cell fuel system

    870

    l

    230

    USgal

    Crew

    Pilots/Passengers

    1/7

    External Dimensions

    Length (rotors turning)

    12.92

    m

    42.37

    ft

    Width (rotor blades at 45°)

    7.76

    m

    25.43

    ft

    Maximum height

    3.60

    m

    11.78

    ft

    Main rotor diameter

    10.83

    m

    35.53

    ft

    Tail rotor diameter

    1.94

    m

    6.36

    ft

    MR tip blade ground clearance

    2.83

    m

    9.3

    ft

    TR tip blade ground clearance

    1.15

    m

    3.77

    ft

    Fuselage ground clearance

    0.63

    m

    2.06

    ft

    Performance (ISA, 2850 kg / 6283 lb)

    VNE

    282

    km/h

    152

    kt

    Max speed

    256

    km/h

    138

    kt

    Rate of climb

    9.4

    m/s

    1850

    ft/s

    Hovering IGE (TOP)

    3352

    m

    11000

    ft

    Hovering OGE (TOP)

    2225

    m

    7300

    ft

    Service ceiling (MCP)

    4572

    m

    15000

    ft

    Max range*

    954

    km

    515

    nm

    Max endurance*

    5 h 20 min

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