AW109 SP GrandNew

LIGHT, TWIN-ENGINE, MULTI-FUNCTIONAL HELICOPTER…
The GRAND helicopters are light and twin-engine helicopters manufactured with latest technology, which have been developed by considering different market demands and ensure large cabin and large baggage feasibilities.

With the capacity of 2 pilots and maximum 6 passengers, the GRAND helicopters are suitable for usage in widely ranging areas such as Corporate VIP transfers; first aid and medical services; search & rescue; security forces, coastal security; and offshore transport.

Equipped with a robust, special fuselage as well as passenger and cockpit seats and FADEC-controlled engines and fuel cells for excellent performance, the GRAND considers safety as the highest priority.

Spacious and long, obstacle-free passenger cabin offering different cabin layout options and long and easily accessible baggage compartment with high load capacity are available.

The GRAND helicopters are environmentally friendly with their low noise level, low fuel consumption and low pollutant emissions. They feature a new design aiming to minimize maintenance costs and contribute to lower operating costs. Also, fixed-cost material support programs provide a wide-scope support for cost efficiency for the user.

WEIGHT
Max Gross Weight (internal loads) 3175 kg
Basic Empty Weight 1655 kg
Max Gross Weight (external loads) 3200 kg
PROPULSION
Pratt&Whitney PW 207C
ENGINE RATING
AEO Take Off Power(5 min) 735 SHP x 2
AEO Maximum continuous power 625 SHP x 2
TRANSMISSION RATING
Take off 960 SHP
Max continuous 900 SHP
CAPACITY
1 Flight Crew + 7 Passenger Seating
2 Flight Crew + 6 Passenger Seating
2 Flight Crew+ 5 Passenger Seating VIP
DIMENTIOS
Lenght (rotors turning) 12.96 m
Height (top of tail fin) 3.44 m
Main rotor clearance 2.45 m
Tail rotor clearance (rotors turning) 1.00 m
BAGGAGE COMPARTMENT 0,90 m³
PERFORMANS
VNE (SL) 311 km/h 168 knot
Max Cruice speed (SL-TOP) 288 km/h 155 knot
Hover IGE 4750 m 15.600 feet
Hover OGE 3050 m 10.000 feet
FUEL CAPACITY
3 – Cell Fuel System 152 USG 460 kg.
4 – Cell Fuel System 177 USG 535 kg.
5 – Cell Fuel System 213 USG 644 kg.
RANGE
Max. Range 800 km 432 mn
Max. Endurance (5 – cell fuel system) 4 :03 h:min