Upgraded version of the CH-47J including larger fuel tank

Overview

Data on design, manufacture and status

Design authority: The Boeing Company

Primary manufacturer: Kawasaki Heavy Industries Ltd.

Parent type: Boeing Model 234/H-47 Chinook

Aircraft status: Operational

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 (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 5.78 m (19.0 ft)

Overall Length: 30.18 m (99.0 ft)

Overall Width: 18.29 m (60.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Lycoming T55-L-712 turbine

Engine manufacturer: Lycoming Engines

Max continuous power: 2797 kW (3749 hp)

Intermediate power: 3356 kW (4499 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Related VFS Resources

Resources related to the CH-47JA , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the CH-47JA , provided by public sources across the internet.

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