- Trained on our vast library of engineering resources.

AgustaWestland Helicopter AW139

Description
The AW139 is the market-leading intermediate twin-engine helicopter - the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world. The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS and benefits from the best-in-class power reserve and outstanding power to weight ratio, which provides Category A performance capabilities with no limitations in a wide range of operating conditions, including ‘hot and high’. Passengers and mission operators benefit from the largest, most comfortable cabin in the intermediate twin-engine class. Leading Features MTOW: 6,400/6,800 kg Powerplant: 2 x Pratt &Whitney Canada PT6C-67C (Take-Off: 1,679 shp) Crew/passengers: 1 or 2 pilots with 15 passengers Technical Data Weights Max Take Off weight (MTOW) 6400 / 6800* kg 14110 / 14991* lb Max useful load 2650 / 3050 kg 5843 / 6724 lb Engine Rating (2 x Pratt & Whitney PT6C - 67C) Take off power (5 min) 2 x 1252 kW 2 x 1679 shp Maximum continuous power 2 x 1142 kW 2 x 1531 shp O.E.I. max contingency power 1396 kW 1872 shp O.E.I. max continuous power 1252 kW 1679 shp Transmission Rating Take off power (5 min) 1641 kW 2200 shp Maximum continuous power 1491 kW 2000 shp O.E.I. min contingency power 1193 kW 1600 shp O.E.I. max continuous power 1044 kW 1400 shp Fuel Capacity Standard 1568 l 414 USgal Auxiliary 500 l 132 USgal Crew Pilots / passengers 1 - 2 / 15 External Dimensions Length (rotors turning) 16.66 m 54 ft 08 in Overall height 4.98 m 16 ft 04 in Main rotor diameter 13.80 m 45 ft 03 in Performance (ISA, 6400 kg / 14110 lb) VNE (SL) 310 km / h 167 kts Max cruise speed (SL) 306 km / h 165 kts Rate of climb (SL) > 10.9 m / s > 2140 ft / min Hovering IGE (TOP) 4682 m 15360 ft Hovering OGE (TOP) 2478 m 8130 ft Service ceiling (MCP) 6096 m 20000 ft Max range ** 1250 km 675 nm Max endurance ** 5 h 56 m * An optional MTOW (Internal) of 6800 kg (14881) lb is available as a kit ** With 1654 kg fuel - no reserve - @ 6000 ft
Datasheet

Suppliers

Company
Product
Description
Supplier Links
Helicopter - AW139 - AgustaWestland
Cascina Costa di Samarate, Varese, Italy
Helicopter
AW139
Helicopter AW139
The AW139 is the market-leading intermediate twin-engine helicopter - the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world. The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS and benefits from the best-in-class power reserve and outstanding power to weight ratio, which provides Category A performance capabilities with no limitations in a wide range of operating conditions, including ‘hot and high’. Passengers and mission operators benefit from the largest, most comfortable cabin in the intermediate twin-engine class. Leading Features MTOW: 6,400/6,800 kg Powerplant: 2 x Pratt &Whitney Canada PT6C-67C (Take-Off: 1,679 shp) Crew/passengers: 1 or 2 pilots with 15 passengers Technical Data Weights Max Take Off weight (MTOW) 6400 / 6800* kg 14110 / 14991* lb Max useful load 2650 / 3050 kg 5843 / 6724 lb Engine Rating (2 x Pratt & Whitney PT6C - 67C) Take off power (5 min) 2 x 1252 kW 2 x 1679 shp Maximum continuous power 2 x 1142 kW 2 x 1531 shp O.E.I. max contingency power 1396 kW 1872 shp O.E.I. max continuous power 1252 kW 1679 shp Transmission Rating Take off power (5 min) 1641 kW 2200 shp Maximum continuous power 1491 kW 2000 shp O.E.I. min contingency power 1193 kW 1600 shp O.E.I. max continuous power 1044 kW 1400 shp Fuel Capacity Standard 1568 l 414 USgal Auxiliary 500 l 132 USgal Crew Pilots / passengers 1 - 2 / 15 External Dimensions Length (rotors turning) 16.66 m 54 ft 08 in Overall height 4.98 m 16 ft 04 in Main rotor diameter 13.80 m 45 ft 03 in Performance (ISA, 6400 kg / 14110 lb) VNE (SL) 310 km / h 167 kts Max cruise speed (SL) 306 km / h 165 kts Rate of climb (SL) > 10.9 m / s > 2140 ft / min Hovering IGE (TOP) 4682 m 15360 ft Hovering OGE (TOP) 2478 m 8130 ft Service ceiling (MCP) 6096 m 20000 ft Max range ** 1250 km 675 nm Max endurance ** 5 h 56 m * An optional MTOW (Internal) of 6800 kg (14881) lb is available as a kit ** With 1654 kg fuel - no reserve - @ 6000 ft

The AW139 is the market-leading intermediate twin-engine helicopter - the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world.

The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS and benefits from the best-in-class power reserve and outstanding power to weight ratio, which provides Category A performance capabilities with no limitations in a wide range of operating conditions, including ‘hot and high’.
Passengers and mission operators benefit from the largest, most comfortable cabin in the intermediate twin-engine class.

Leading Features

MTOW: 6,400/6,800 kg

Powerplant: 2 x Pratt &Whitney Canada PT6C-67C (Take-Off: 1,679 shp)

Crew/passengers: 1 or 2 pilots with 15 passengers

Technical Data

Weights

Max Take Off weight (MTOW)6400 / 6800*kg14110 / 14991*lb
Max useful load2650 / 3050kg5843 / 6724lb

Engine Rating (2 x Pratt & Whitney PT6C - 67C)

Take off power (5 min)2 x 1252kW2 x 1679shp
Maximum continuous power2 x 1142kW2 x 1531shp
O.E.I. max contingency power1396kW1872shp
O.E.I. max continuous power1252kW1679shp

Transmission Rating

Take off power (5 min)1641kW2200shp
Maximum continuous power1491kW2000shp
O.E.I. min contingency power1193kW1600shp
O.E.I. max continuous power1044kW1400shp

Fuel Capacity

Standard1568l414USgal
Auxiliary500l132USgal

Crew

Pilots / passengers1 - 2 / 15

External Dimensions

Length (rotors turning)16.66m54ft08in
Overall height4.98m16ft04in
Main rotor diameter13.80m45ft03in

Performance (ISA, 6400 kg / 14110 lb)

VNE (SL)310km / h167kts
Max cruise speed (SL)306km / h165kts
Rate of climb (SL)> 10.9m / s> 2140ft / min
Hovering IGE (TOP)4682m15360ft
Hovering OGE (TOP)2478m8130ft
Service ceiling (MCP)6096m20000ft
Max range **1250km675nm
Max endurance **5 h 56 m

* An optional MTOW (Internal) of 6800 kg (14881) lb is available as a kit
** With 1654 kg fuel - no reserve - @ 6000 ft

Supplier's Site Datasheet

Technical Specifications

  AgustaWestland
Product Category Aircraft
Product Number AW139
Product Name Helicopter
Unlock Full Specs
to access all available technical data

Similar Products