Gunship version of the CH-47A

Overview

Data on design, manufacture and status

Design authority: The Boeing Company

Primary manufacturer: The Boeing Company

Parent type: Boeing Model 234/H-47 Chinook

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Tandem (Fore/aft) (x2)

Crew required: 2

Crew seating: Side-by-side

Landing gear: Wheels (some retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 5.68 m (18.7 ft)

Overall Length: 29.90 m (98.1 ft)

Overall Width: 18.01 m (59.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Lycoming T55-L-7 turbine

Engine manufacturer: Lycoming Engines

Take-off / rated power: 1977 kW (2650 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 14969 kg (33000 lb)

Max Range: 1344 km (726 nm)

Related VFS Resources

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Related Public Resources

Resources related to the ACH-47A Chinook, provided by public sources across the internet.

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