aircraft
Manufacturer:
| Airbus Helicopters | |
Country:
| Europe | |
Commercial designation:
| Tigre | |
Technical designation:
| EC665 | |
Version, Variant:
| HAP | |
Type:
| Conventional | |
Currently produced:
| Y | |
Typical missions:
| Military Combat Attack | |
Flight conditions:
| IFR | |
First flight:
| 1991 | |
Landing system:
| wheels | |
Blades number:
| 4 | |
Tail blades number:
| 3 | |
weight
Weight class:
| 4 | |
MTOW with external loads:
| 6100 kg | 13451 lbs |
MTOW with only internal loading:
| 0 kg | 0 lbs |
Empty weight:
| 4200 kg | 9261 lbs |
External payload:
| 1800 kg | 3969 lbs |
Internal payload:
| 0 kg | 0 lbs |
Standard fuel tank:
| 1105 kg | 2437 lbs |
with optionnal external fuel tank:
| 1689 kg | 3724 lbs |
performance
Cruise speed:
| 230 km/h | 124 kt |
Maximum cruise speed:
| 278 km/h | 150 kt |
Vne:
| 322 km/h | 174 kt |
Max negative g @ MTOW:
| 0 g | |
Max positive g @ MTOW:
| 0 g | |
Range with normal tanks:
| 800 km | 432 nm |
Max range with auxiliary external tanks:
| 1280 km | 691 nm |
Max endurance @ min consumption speed:
| 03:25:00 h:min | |
Rate of climb @ SL:
| 11.5 m/s | 2263 ft/min |
Rate of climb @ SL @MTOW:
| 0 m/s | 0 ft/min |
IGE max hovering altitude, MTOW:
| 0 m | 0 ft |
IGE max hovering altitude, empty:
| 0 m | 0 ft |
IGE max hovering altitude, ISA+20°C, MTOW:
| 0 m | 0 ft |
IGE max hovering altitude, ISA+20°C, empty:
| 0 m | 0 ft |
OGE max hovering altitude, MTOW:
| 3500 m | 11480 ft |
OGE max hovering altitude, empty:
| 0 m | 0 ft |
OGE max hovering altitude, ISA+20°C, MTOW:
| 0 m | 0 ft |
OGE max hovering altitude, ISA+20°C, empty:
| 0 m | 0 ft |
Service ceiling ISA, MTOW:
| 4000 m | 13120 ft |
Max operating altitude, empty weight:
| 0 m | 0 ft |
Highest use Temperature:
| 35 °C | 63 °F |
Lowest use Temperature:
| -30 °C | -54 °F |
power
APU in HC:
| ||
Engine manufacturer:
| Turbomeca | |
Model:
| MTR 390 | |
Engines quantity:
| 2 | |
Powerplant category:
| turbine | |
Main rotor rotation speed:
| 0 rpm | |
Fuel consumption @ SL @ max continuous speed:
| 0 kg/kW/h | 0 lbs/hp/h |
Minimum consumption speed @ SL:
| 0 km/h | 0 kt |
Fuel consumption @ eco cruise speed @SL:
| 0 kg/h | 0 lbs/h |
Fuel consumption @ min consumption speed @ SL:
| 0 kg/h | 0 lbs/h |
Engines nominal power:
| 1746 kW | 2373 hp |
Transmission shaft max continuous power:
| 0 kW | 0 hp |
Transmission shaft max power:
| 0 kW | 0 hp |
Takeoff power 5 min:
| 1936 kW | 2631 hp |
OEI 30s power:
| 1160 kW | 1576 hp |
OEI 2min power:
| 0 kW | 0 hp |
OEI max continuous power :
| 0 kW | 0 hp |
OEI max continuous transmission power:
| 0 kW | 0 hp |
OEI 30 sec transmission power:
| 0 kW | 0 hp |
OEI 2 min transmission power:
| 0 kW | 0 hp |
dimensions
Overall length:
| 15.82 m | 52 ft |
Rotor diameter:
| 13 m | 43 ft |
Tail rotor diameter:
| 2.7 m | 9 ft |
Fuselage length:
| 14.27 m | 47 ft |
Overall height:
| 4.32 m | 14 ft |
Main rotor blades chord:
| 0 m | 0 ft |
Tail rotor blades chord:
| 0 m | 0 ft |
Mast tilt angle:
| 0 ° | |
noise
Noise at flyover, level:
| 0 dB EPNL | |
Noise at flyover, limit:
| 0 dB EPNL | |
Noise at takeoff, level:
| 0 dB EPNL | |
Noise at takeoff, limit:
| 0 dB EPNL | |
Noise at landing, level:
| 0 dB EPNL | |
Noise at landing, limit:
| 0 dB EPNL | |
seating
Crew:
| 2 | |
Max pax number:
| 0 | |
use
Average price:
| 3.2e+07 $ | |
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