- Trained on our vast library of engineering resources.

AgustaWestland Helicopter AW119Kx

Description
The AW119Kx is the most spacious and powerful light single-engine helicopter for a wide range of missions. Government and commercial operators benefit from the highest levels of mission flexibility and productivity at competitive procurement and operating costs. A modern glass cockpit configured with Garmin’s G1000H(TM) 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 and separate baggage compartment permits rapid reconfiguration for a variety of missions. High power margins provide the performance capability to deliver excellent flying qualities, high controllability and manoeuvrability, combined with the robust, inherent ‘fail safe’ design and redundancy of main systems, operators confidence is assured. Leading Features MTOW: 2,850 kg Powerplant: 1 x Pratt & Whitney PT6B-37A (Take-Off: 1,002 shp) Crew/passengers: 1 or 2 pilots with 7 or 6 passengers Technical Data 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 1-2 / 7-6 External Dimensions Length (rotors turning) 12.92 m 42 ft 05 in Width (rotor blades at 45°) 7.76 m 25 ft 05 in Maximum height 3.60 m 11 ft 10 in Main rotor diameter 10.83 m 35 ft 06 in Tail rotor diameter 1.94 m 6 ft 04 in MR tip blade ground clearance 2.83 m 9 ft 03 in TR tip blade ground clearance 1.15 m 3 ft 09 in Fuselage ground clearance 0.63 m 2 ft 01 in Performance (ISA, 2850 kg / 6283 lb) VNE 282 km/h 152 kt Max speed 244 km/h 131 kt Rate of climb 9.1 m/s 1800 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 * with 230 USgal fuel - no reserve - @ 5000 ft
Datasheet

Suppliers

Company
Product
Description
Supplier Links
Helicopter - AW119Kx - AgustaWestland
Cascina Costa di Samarate, Varese, Italy
Helicopter
AW119Kx
Helicopter AW119Kx
The AW119Kx is the most spacious and powerful light single-engine helicopter for a wide range of missions. Government and commercial operators benefit from the highest levels of mission flexibility and productivity at competitive procurement and operating costs. A modern glass cockpit configured with Garmin’s G1000H(TM) 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 and separate baggage compartment permits rapid reconfiguration for a variety of missions. High power margins provide the performance capability to deliver excellent flying qualities, high controllability and manoeuvrability, combined with the robust, inherent ‘fail safe’ design and redundancy of main systems, operators confidence is assured. Leading Features MTOW: 2,850 kg Powerplant: 1 x Pratt & Whitney PT6B-37A (Take-Off: 1,002 shp) Crew/passengers: 1 or 2 pilots with 7 or 6 passengers Technical Data 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 1-2 / 7-6 External Dimensions Length (rotors turning) 12.92 m 42 ft 05 in Width (rotor blades at 45°) 7.76 m 25 ft 05 in Maximum height 3.60 m 11 ft 10 in Main rotor diameter 10.83 m 35 ft 06 in Tail rotor diameter 1.94 m 6 ft 04 in MR tip blade ground clearance 2.83 m 9 ft 03 in TR tip blade ground clearance 1.15 m 3 ft 09 in Fuselage ground clearance 0.63 m 2 ft 01 in Performance (ISA, 2850 kg / 6283 lb) VNE 282 km/h 152 kt Max speed 244 km/h 131 kt Rate of climb 9.1 m/s 1800 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 * with 230 USgal fuel - no reserve - @ 5000 ft

The AW119Kx is the most spacious and powerful light single-engine helicopter for a wide range of missions.

Government and commercial operators benefit from the highest levels of mission flexibility and productivity at competitive procurement and operating costs.

A modern glass cockpit configured with Garmin’s G1000H(TM) 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 and separate baggage compartment permits rapid reconfiguration for a variety of missions.

High power margins provide the performance capability to deliver excellent flying qualities, high controllability and manoeuvrability, combined with the robust, inherent ‘fail safe’ design and redundancy of main systems, operators confidence is assured.

Leading Features

MTOW: 2,850 kg

Powerplant: 1 x Pratt & Whitney PT6B-37A (Take-Off: 1,002 shp)

Crew/passengers: 1 or 2 pilots with 7 or 6 passengers

Technical Data

Weights

Max take off (int. loads)2850kg6283lb
Max take off (ext. loads)3150kg6945lb
Basic empty weights1483kg3269lb

Engine Rating (Pratt & Whitney PT6B-37A)

Take off747kW1002shp
Maximum continuous power650kW872shp

Transmission Rating

Take off684kW917shp
Maximum continuous power671kW900shp

Fuel Capacity

3-cell fuel system605l160USgal
4-cell fuel system711l188USgal
5-cell fuel system870l230USgal

Crew

Pilots / Passengers1-2 / 7-6

External Dimensions

Length (rotors turning)12.92m42ft05in
Width (rotor blades at 45°)7.76m25ft05in
Maximum height3.60m11ft10in
Main rotor diameter10.83m35ft06in
Tail rotor diameter1.94m6ft04in
MR tip blade ground clearance2.83m9ft03in
TR tip blade ground clearance1.15m3ft09in
Fuselage ground clearance0.63m2ft01in

Performance (ISA, 2850 kg / 6283 lb)

VNE282km/h152kt
Max speed244km/h131kt
Rate of climb9.1m/s1800ft/s
Hovering IGE (TOP)3352m11000ft
Hovering OGE (TOP)2225m7300ft
Service ceiling (MCP)4572m15000ft
Max range*954km515nm
Max endurance*5 h 20 min

* with 230 USgal fuel - no reserve - @ 5000 ft

Supplier's Site Datasheet

Technical Specifications

  AgustaWestland
Product Category Aircraft
Product Number AW119Kx
Product Name Helicopter
Unlock Full Specs
to access all available technical data

Similar Products