Helicopter • Boeing • CH-47A, CH-47D, CH-47F, MH-47E, CH-47i
| Manufacturer | Boeing |
| Model | CH-47 Chinook |
| Category | Helicopter |
| Variants | CH-47A, CH-47D, CH-47F, MH-47E, CH-47i |
| Seating | 44, 55 seats |
| Typical TTAF | 8,500 hours |
| Markets | United States, United Kingdom, Canada, Germany, Australia |
| Price Range | $8.0M – $52.0M |
The Boeing CH-47 Chinook is a heavy-lift cargo helicopter that has served as a cornerstone of military aviation for over six decades. Recognizable by its distinctive dual rotor system—one at the nose and one at the tail—the Chinook delivers exceptional lifting capacity and reliability in demanding operational environments. Originally developed in the 1960s, it has become the primary heavy-lift helicopter for the United States Army and is operated by 19+ nations worldwide. The aircraft excels in troop transport, cargo operations, medical evacuation, and disaster relief missions. Its tandem rotor configuration eliminates the need for a tail rotor, providing superior stability and allowing it to carry external loads up to 26,000 pounds. The Chinook's proven design, continuous modernization, and unmatched payload capacity make it indispensable for military logistics and humanitarian operations globally. Modern variants feature advanced avionics, improved engines, and enhanced survivability features, ensuring relevance in contemporary operations.
Maximum Speed: 170 knots (196 mph)
Cruise Speed: 150 knots (173 mph)
Range: 1,200 nautical miles
Service Ceiling: 15,000 feet
Maximum Takeoff Weight: 50,000 lbs
Engines: Two Lycoming T55-L-712 turboshafts (4,733 shp each)
Payload Capacity: 26,000 lbs external, 12,000 lbs internal
Rotor Diameter: 60 feet (each)
Length: 98.23 feet
Cabin Width: 7.67 feet