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CH-47F Chinook

CH-47F Chinook

Utility & Transport Helicopters
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Basic Information
Name
CH-47F Chinook
Designation
CH-47F Chinook
Alternate Designation
CH-147F Chinook (Canada), Chinook Mk6 (Royal Air Force), ICH-47F Chinook (Italian Army)
Equipment Type
Utility & Transport Helicopters
Manufacturer
Boeing
Date of Introduction
2006
Description

The CH-47F is an upgraded model of proven CH-47D Chinook helicopter. The new Chinook model features reduced vibration effects, an integrated cockpit control system, and more powerful T55-GA-714A engines fitted with digital fuel control. Each engine is rated at 4,868 horsepower (shp). The US Army plans to upgrade up to 300 existing CH-47Ds to the F configuration with the first delivery due in 2004. Entry into service is expected in 2006. The CH-47Fs will remain in service well beyond 2030. They should start enter retirement beginning in 2035. As of January 2005, the latest US Army's acquisition plan approved the increase of the Chinook fleet from 463 to 513 aircraft. The plan included upgrade of the entire fleet of 397 CH-47Ds to the F-model configuration and acquisition of at least 55 additional new-build CH-47Fs. The US Special Operations Command will increase their current fleet of 34 MH-47D/E special operations heavy assault Chinooks to 61 MH-47Gs, with options on further aircraft. As of April 2008, overall value of the CH-47F program was set at $13.35 billion for approximately 513 helicopters. The first production CH-47F helicopter was unveiled by Boeing in June 2006.

Air & Air Defense Specifications
Crew 3
Max Speed 281.6 km/h
Range 740.8 km
Overview (Deagel)
Group Utility & Transport Helicopters
Status Active
Also Known As CH-147F Chinook (Canada), Chinook Mk6 (Royal Air Force), ICH-47F Chinook (Italian Army)
Origin United States of America
Contractor Boeing
Initial Operational Capability (IOC) 2006
Total Production 243
Unitary Cost USD $42 million
Specifications (Deagel)
Crew 3
Main Rotor Blades 6
Number of Engines 2
Troops 33
Dimensions — Height 5.5 meter
Dimensions — Length 30.2 meter
Dimensions — Main Rotor Diameter 18.3 meter
Dimensions — Width 3.6 meter
Mass — Empty Weight 10,615 kilogram
Mass — Max Takeoff Weight 22,680 kilogram
Mass — Payload 21,000 pound
Performance — Radius of Operation 400 nautical mile
Power — Max Power at TakeOff 9,466 hp
Speed — Cruise Speed 265 kph
Speed — Top Speed at High Altitude 175 mph
Gear (Deagel)
Item 1 ESM & Warning Systems: AN/AAR-57 CMWS (1)
Item 2 Jamming Systems: AN/AAQ-24 Nemesis
Item 3 Jamming Systems: AN/ALQ-212 ATIRCM (1)
Item 4 Jamming Systems: CIRCM
Item 5 Turboshaft Engines: T-55-GA-714A (2)
Variants
Variant 1 CH-47D Chinook
Variant 2 MH-47E Chinook
Variant 3 MH-47G Chinook
Variant 4 CH-47F Chinook
Variant 5 HH-47 Chinook
Variant 6 MH-47G Block II Chinook
Variant 7 CH-47F Block II Chinook
Details
Country of Origin United States
Category Transport Helicopter
Air > Transport Helicopter
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
30.2 m
Width
Height
5.5 m
Weight
22680 kg
Related Equipment (1)
Operators (12)
United States
United Kingdom
Italy
South Korea
India
Spain
Australia
Canada
Egypt
Netherlands
Saudi Arabia
United Arab Emirates
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