| Name / Designation | CH-47F Chinook |
| Type / Role | Heavy-Lift Transport Helicopter |
| Country of Origin | United States |
| Manufacturer | Boeing Defense, Space & Security |
| Introduced / Service Entry | 2007 |
| Operational Status | Active |
| Operators | USA, UK, Australia, Netherlands, others |
| Maximum Speed (Road) | ~315 km/h |
| Cruise Speed | ~290 km/h |
| Range | ~740 km (combat) / ~1,200 km (ferry) |
| Endurance | ~3–4 hours |
| Service Ceiling | ~6,100 m |
| Rate of Climb | ~7.6 m/s |
| Length | 30.1 m |
| Height | 5.7 m |
| Rotor Diameter | 18.3 m (each rotor) |
| Empty Weight | ~10,200 kg |
| Maximum Takeoff Weight (MTOW) | ~22,680 kg |
| Primary Armament | M240 / M134 door-mounted machine guns |
| Secondary Armament | None (defensive only) |
| Hardpoints / Weapon Stations | N/A |
| Payload Capacity | Up to 10,000+ kg |
| Countermeasures | Flares, Chaff, ECM |
| Radar Name | Weather / Navigation Radar |
| Targeting System | NVG-compatible cockpit |
| Navigation System | GPS / INS |
| Communication System | Secure radios, data link |
| Defensive Systems | MAWS / RWR |
| Engines | 2 × Turboshaft |
| Engine Model | Honeywell T55-GA-714A |
| Power Output | ~4,868 shp each |
| Fuel Capacity | ~3,900 L |
| Crew | 3 (Pilot, Co-Pilot, Flight Engineer) |
| Passenger Capacity | 33–55 troops |
| Cabin Configuration | Troop / Cargo / MEDEVAC |
| Cargo Load (Internal/External) | Internal & External Sling |
| Mission Types | Transport, Logistics, MEDEVAC, SAR |
| Night Operation Capability | Yes |
| All-weather Operation | Yes |
| Combat Proven | Yes |
The CH-47F Chinook Heavy-Lift Transport Helicopter is one of the most capable and battle-proven military transport helicopters in active service today. Designed for demanding battlefield logistics, the CH-47F provides the U.S. Army and allied forces with unmatched heavy-lift, troop transport, and disaster-response capabilities.
Manufactured by Boeing Defense, Space & Security, the CH-47F is the latest production variant of the iconic Chinook family, originally developed in the United States during the Cold War. Entering service in the mid-2000s, the F-model introduced a modernized digital cockpit, improved airframe durability, and more powerful engines to support 21st-century operations.
Powered by twin Honeywell T55-GA-714A turboshaft engines, the CH-47F delivers exceptional lift performance, even in hot-and-high environments. It can transport over 33 fully equipped troops, evacuate casualties, or carry heavy cargo internally or as an external sling load exceeding 10,000 kg. With a cruise speed near 290 km/h and long-range ferry capability, the Chinook excels in rapid force mobility.
The helicopter features an advanced Common Avionics Architecture System (CAAS) with digital flight controls, moving-map displays, GPS/INS navigation, and secure communications. Survivability is enhanced through missile warning systems, radar warning receivers, ballistic protection, and countermeasure dispensers.
The CH-47F has seen extensive service in Iraq, Afghanistan, and humanitarian relief missions worldwide, proving its reliability in combat, logistics, and disaster response roles. It remains a cornerstone of U.S. Army aviation and a preferred heavy-lift platform among NATO allies.
The unit cost of a CH-47F Chinook typically ranges between USD 35–40 million, depending on configuration, avionics packages, training, and support agreements.
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