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Quintus Technologies Quintus Technologies
ProgramsBoeing CH-47 Chinook

Aircraft program

Boeing CH-47 Chinook

In production
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A medium to heavy-lift helicopter primarily for cargo - transport of troops, weapons, equipment and fuels but also humanitarian missions.

Powered by two rear mounted turboshaft Honeywell engines connected by drive shafts to two, counter-rotating, 3 blade rotors made from composite materials with tapered tips to increase stability and enhance handling capabilities. Designed for advanced cargo capability with rear loading ramp, three underslung external cargo hooks and large internal space for freight or up to 55 troops.

2 pilots in advanced digital cockpit face LCD displays and dual, digital automatic flight controls. Jumps seats for 1 or 2 support crew.

Chinooks serve the defence forces in 19 countries.

Lift type
Rotary wing
Construction
Factory-built
Control
Piloted
Engine type
Turboshaft
Application
Military transport, Utility
Final assembly

Design & construction

Primary structure
Aluminium
Landing gear
Fixed tricycle
Ice protection
None
Pressurisation
Unpressurised
Flight controls
Hydro-mechanical
Autopilot
3-axis
Avionics architecture
Integrated glass suite
Environmental control
None-unpressurised
Rotor configuration
Tandem
Certification
Military
Minimum crew
2

Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.

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Type variants

VariantLaunch / first flightProduction endNotes
Boeing CH-47D1976 / 19792021Variant with modernised engines compared to prior models.
Boeing CH-47J1986 / 1986Japanese variant for JGSDF and JASDF, includes upgraded CH-47JA variant.
Boeing CH-47F2001 / 2001Production: 1 (2018) GAMA: Leonardo Helicopters CH47F. Upgraded CH-47D variant.
Boeing MH-47G2002 / 2002Special Operations variant, includes prior variants MH-47D/E.

Airframer

Boeing Defense, Space & SecurityNews
Kawasaki AerospaceLicenced production of CH-47JA variant

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Program milestones 63 dated events

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Information on this page is compiled from a variety of published sources; links do not necessarily imply recommendation or confirmation by the airframe manufacturer.

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