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Boeing CH-47F Chinook

2001 · Twin-engine heavy turbine helicopter

History C/N Operators News
Aimed as a low cost re-manufacture of the CH-47D and to extend the model life to 2060, the CH-47F first flew in 2001 and the first production machine came off the Boeing Pennsylvania line in July 2004.

All F-models are built with a completely re-designed and newly manufactured airframe. While some aircraft are assembled with “recycled” components from D-models, approximately 40 of the F-models produced as of 2014 are “new builds”.

Main features includes new 4.868 shp Honeywell engines, improved avionics and an upgraded airframe with larger single-piece sections to reduce part count thus reducing vibrations and the need for inspections and repairs.

Specifications

Engine2 x Lycoming T55-GA-714A 4868 shp
Capacity3 + 55
Length (m)15.9
Height (m)5.77
Blades3
Rotor diam. (m)18.29
Disc area (m2)260
Weight (kgs)Empty: 10100 Max: 22600
Speed (km/h)Cruise: 220 Max: 315
Range (km)740
Ceiling (m)5600
Rate/Climb (m/min)463
blueprints CH-47F Chinook

Derivatives & Versions

MH-47G Chinook 2004 Based on the CH-47F with the CAAS glass cockpit, the MH-47G Special Operations Aircraft (SOA) are used by 160th SOAR.
HH-47H Chinook 2006 The HH-47, a variant based on the special operations aircraft MH-47G, was selected by the USAF as the winner of the Combat Search and Rescue ( CSAR-X ) competition on November 2006 against the AgustaWestland HH-71 in procure of 141 aircraft to replace its ageing fleet of HH-60G Page Hawks.
CH-147F Chinook 2012 CH-47F variant for the Canadian Forces.
ICH-47F Chinook 2013 AgustaWestland and Boeing signed an industrial agreement for the joint manufacture of the ICH-47F in July 2008.
CH-47F Block II 2019 The CH-47F Block II Chinook featured an improved drivetrain to transfer greater power from the engines to the all-new, swept-tip Advanced Chinook Rotor Blades, which have been engineered to lift 1,500 additional pounds on their own.