A.109 with one Pratt & Whitney PT6B-37/1 turboshaft engine, fixed skid u/c. Prot. I-KOAL FF Feb. 1995.

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Technical data for Agusta A119 Crew: 1, passengers: 7, Engine: 1 x Pratt & Whitney Canada PT6B-37 turboshaft, take-off power capacity: 747kW, max continuous power capacity: 650kW, main rotor diameter: 11.00m, length with rotors turning: 13.10m, fuselage length: 11.07m, height: 3.30m, take-off weight: 2600-2850kg, internal payload: 1200kg, external payload: 1320kg, max speed: 278km/h, cruising speed: 260km/h, service ceiling: 5460m, hovering ceiling, OGE: 2450m, hovering ceiling, IGE: 3320m, range: 655km, endurance: 2h 45min

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