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Boeing Vertol H-47 Chinook Family

The CH-47 Chinook is a tandem-rotor heavy-lift helicopter family developed by Vertol and continued by Boeing. Its large cabin, rear loading ramp, external-load capability, and paired rotors support troop and cargo transport, evacuation, disaster relief, firefighting, and specialized civil and military missions. Repeated remanufacturing and digital upgrades have kept the design in production and service with operators around the world for more than six decades.

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Identity

Aliases
CH-47H-47ChinookYCH-1BCH-47ACH-47DCH-47FMH-47GBoeing Model 234
Family Name
Boeing CH-47 Chinook
Full Name
Boeing Vertol H-47 Chinook Family
Roles
cargoutilitymilitarysearch_and_rescueair_ambulancefirefighting
Status
active
Type
aircraft

Details

Aircraft Specs
Configuration
rotorcraft
Operating Modes
land
Takeoff Landing Capabilities
vtol
Description
The CH-47 Chinook is a tandem-rotor heavy-lift helicopter family developed by Vertol and continued by Boeing. Its large cabin, rear loading ramp, external-load capability, and paired rotors support troop and cargo transport, evacuation, disaster relief, firefighting, and specialized civil and military missions. Repeated remanufacturing and digital upgrades have kept the design in production and service with operators around the world for more than six decades.
First Flight Year
1,961
Manufacturer
Propulsion Configurations
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Two exact Honeywell T55-GA-714A turboshaft engines; Boeing and Army sources identify this installation on CH-47F.
    Name
    CH-47F T55-GA-714A installation
    Notes
    Applies only to the CH-47F branch within the broader CH-47 family record; CH-47A/D, MH-47G, commercial Model 234, and later T55-714C configurations remain separately modeled.
  • Entries
    • Count
      2
      Propulsion System
      Role
      main
      Variant Notes
      The Department of the Army identifies CH-47D aircraft as affected by conversion of T55-L-712 engines to T55-GA-714A configuration; the Army's CH-47 procurement context describes the heavy-lift helicopter as powered by two T55 turbine engines. Placement and stage are left unspecified because the cited evidence does not state them.
    Name
    CH-47D T55-L-712 installation
    Notes
    Historical CH-47D branch before the Army's T55-GA-714A conversion program.

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Creation Time
July 29, 2026 at 12:11:45 UTC
Updated Time
August 14, 2026 at 17:10:34 UTC