This was the prototype of the A1019 Type series. 1 pilot + 7 PAX for VFR operations.

An excellent description of the aircraft can be found in the following reference,

Source: "Agusta A.109 Hirundo", FLIGHT International, 25 January 1971, Pages 127-130

Overview

Data on design, manufacture and status

Design authority: Leonardo S.p.A, Helicopter Division

Primary manufacturer: Costruzioni Aeronautiche Giovanni Agusta

Parent type: AgustaWestland A109/AW109

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 11.00 m (36.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Allison 250-C20 turbine

Engine manufacturer: Allison Engine Company

Take-off / rated power: 298 kW (400 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2450 kg (5401 lb)

Max Range: 680 km (367 nm)

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