Combat support version. Early Delivery Configuration (EDH)

Overview

Data on design, manufacture and status

Design authority: AgustaWestland N.V.

Primary manufacturer: AgustaWestland N.V.

Parent type: AgustaWestland A129/AW129

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Tandem

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 3.40 m (11.2 ft)

Overall Width: 11.90 m (39.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: RR CTS800-4A turbine

Engine manufacturer: Rolls-Royce

Take-off / rated power: 1014 kW (1359 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 5000 kg (11023 lb)

Max Range: 1000 km (540 nm)

Max Endurance: 3.0 hrs (3.0 hrs)

Related VFS Resources

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Related Public Resources

Resources related to the T129A , provided by public sources across the internet.

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