Sometimes referred to as Chinook Mark 6. A derivative of the CH-47F.

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: 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: Honeywell T55-L-714A turbine

Engine manufacturer: Honeywell Aerospace

Max continuous power: 3039 kW (4074 hp)

Take-off / rated power: 3631 kW (4867 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 22980 kg (50661 lb)

Related VFS Resources

Resources related to the HC.6 Chinook, provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the HC.6 Chinook, provided by public sources across the internet.

Images