Products
AW139
The AW139 is a new generation medium twin-turbine helicopter setting new standards against which all medium twins are measured. Designed with inherent multi-role capability and flexibility of operation, the AW139 is capable of carrying up to 15 passengers at very high speed, in a most spacious and comfortable cabin. The ample baggage compartment is accessible both from the cabin and externally. The AW139 provides the best power reserve of any helicopter in the medium twin-engine class. A brand new helicopter, it fully complies with the latest stringent requirements in terms of performance and safety. Its Pratt & Whitney Canada PT6C-67C turbines, together with a state-of-the-art 5-bladed main rotor, deliver a high cruise speed even in demanding conditions at all weights. They deliver an outstanding power to weight ratio, which allows Category “A” performance capabilities with no limitations in a wide range of operating conditions including ‘hot and high’. Leading edge technology includes a Honeywell Primus Epic fully integrated avionics system, a 4-axis digital AFCS and large flat panel colour displays in the cockpit. Full icing protection is available as an option. As a result of the new design approach the AW139 uses fewer components, benefits from integrated avionics and provides easy accessibility to all systems for simplified maintenance tasks. The AW139 can be used for a wide range of applications including executive/VIP transport, EMS/SAR, offshore OGP support, fire fighting, law enforcement, paramilitary and military roles.
| Weights | ||||
|---|---|---|---|---|
| Max take off | 6400 / 6800* | kg | 14110 / 14991* | lb |
| Max useful load | 2680 | kg | 5909 | 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. max 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 | 54.66 | ft |
| Overall height | 4.99 | m | 46.37 | ft |
| Main rotor diameter | 13.80 | m | 42.58 | ft |
| Performance (ISA, 6400 kg / 14110 lb) | ||||
|---|---|---|---|---|
| VNE | 310 | km / h | 167 | kts |
| Max cruise speed | 306 | km / h | 165 | kts |
| Rate of climb | > 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 | |||
* 6800 kg / 14881 lb with the application of the "Bollettino Tecnico N. 139 - 1 - 40
** with 1654 kg fuel - no reserve - @ 6000 ft
- Engine air particle separators
- Closed circuit refuelling system
- Auxiliary fuel tanks (500 litres / 132 USgal)
- Anti/de-icing system
- Wire strike protection
- Blade folding
- Cargo hook
- Single/dual rescue hoist (272 kg / 600 lb) with utility hoist light
- Fast roping/rappelling
- Cargo hook (2200 kg / 4850 lb) with monitoring cameras
- External loudspeaker
- Self contained EMS/MEDEVAC kit
- Snow skis/slump protection pads
- Cabin bubble windows
- Life rafts
- Search lights
- Marking for high visibility main rotor blades
- Emergency floats
- Customising painting scheme with metallic colours
- All weather covers
- Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR)
- Weather radar
- Weather/search radar
- 4-axis Digital Automatic Flight Control System (DAFCS) with SAR modes & FMS SAR patterns
- Health and Usage Monitoring System (HUMS)
- Helicopter Operations Monitoring Programme (HOMP)
- NVG compatibility (cockpit & external lights)
- SATCOM Iridium satellite phone
- TCAS I
- FLIR
- Digital video recorder
- Video downlink
- Helicopter Emergency Exit Light System (HEELS)
- Auto-Deployable ELT (ADELT)
- Moving map on 5th display
- Enhanced Ground Proximity Warning System (EGPWS)
- Enhanced Vision System (EVS)
- HF radios
- Tactical radios
- Maritime radios
- Executive interior
- VIP interior
- Elite interior
- EMS interior
- SAR interior
- Law enforcement interior
- Air conditioning
- Active Noise Reduction (ANR) headsets
- Silent/Super silent soundproofing
- High density utility kit configuration (15 passengers)
- Cockpit/cabin separation wall
- Passenger Address (PA) system
- Electrically operated passenger steps (left and right)
- Cabinets
- Multi-purpose cubby
- Audio/video entertainment systems with LCD monitors
- VIP interphone system with secure communications
8.25 +1.73%



