AGUSTA A109

The Agusta A109 (renamed AW109) is a light eight-seat twin-engine multi-purpose helicopter produced by the Italian manufacturer Agusta (today AgustaWestland) since 1971. The A109 is used by both civil and military operators.

Specifications & Dimensions

Crew 1-2
Passengers 6-7
Propulsion 2 Turboshaft Engines
Engine Model Allison 250-C20B
Engine Power (each) 313 kW 420 shp
max. Cruise Speed 278 km/h 150 kts
173 mph
max. Speed (vne) 311 km/h 168 kts
193 mph
Service Ceiling 4.572 m 15.000 ft
Rate of climb 503 m/min 1650 ft/min
Range 948 km 512 NM
589 mi.
Empty Weight 1.418 kg 3.126 lbs
max. Takeoff Weight 2.600 kg 5.732 lbs
Rotor Blades (main/tail) 4/2
Main Rotor Diameter 11,00 m 36 ft 1 in
Tail Rotor Diameter 2,03 m 6 ft 8 in
Rotor Disc Area 95,0 m² 1023 ft²
Length (Fuselage) 11,45 m 37 ft 7 in
Length 13,04 m 42 ft 9 in
Height 3,40 m 11 ft 2 in
First Flight 04.08.1971
Production Status in production
ICAO Code A109
IATA Code AGH
FAA TCDS H7EU
EASA TCDS R.005
Data for (Version) Agusta A109A Mk II
Variants A109LUH, A109 Power, A109S Grand

Address

Security Gate 1, Malta International Airport, Luqa LQA 4000, Malta

Telephone

+356 99682666
+356 77016226

Email

info@maltahelicopter.com

Registered Office: Apartment 2, 30 Triq Is-Sorijiet, St. Julians, Malta