[Sign in]   [Why Join]   [Become a member]
  Global Aircraft -- CH-47 Chinook
 
 |  Suggest Changes to Page  | Print this Page 
Aviation Center
  Airbus
  Antonov
  Boeing
  Kamov
  MiG
  Mil
  Saab
  Sukhoi
  Tupolev
Entertainment Center
    About Us
    Definitions
    GAC Times
    G.A. TV
    GAC Forum
    GAC Games
    Help Pages
    Promote GAC
    Site Map
    User Login
Contact Us
    Write To Us

Extra Navigation
GAC Engine
  






CH-47 Chinook
Specifications | Achievements | Photos

CH-47 Chinook


CH-47 Chinook Specifications
Primary Function: Medium-lift helicopter
Contractor: Boeing
Crew: Cockpit-crew seats: 2
Cabin-troop seats/litters: 33/24
Unit Cost: N/A
Powerplant
  Two Textron Lycoming T55-L-712 turboshafts each rated at 3,750 shp for takeoff and 3,000 shp for coninuous running
Dimensions
Length: 98ft 10.75 in
Rotor Diameter: 60 feet (18.29 m) each -- CH-47D
Height: 18 ft 11 in
Weights
Empty: 22,379 lb
Maximum Takeoff: 50,000 lb
Performance
Speed: 159 mph (cruising)
Ceiling: 22,100 ft
Range: N/A
Armament
  N/A
^ Top ^


CH-47 Chinook Achievements
  • During Desert Storm the CH-47D often provided the only means of transportation to shift large numbers of personnel, equipment, and supplies quickly.
^ Top ^


CH-47 Chinook Photos
CH-47 ChinookCH-47 Chinook
CH-47 ChinookCH-47 Chinook
^ Top ^




Top Of Page




Stumble This! Stumble This!    Bookmark on Delicious Bookmark on Delicious!


  Copyright © 2000-2022,   The Global Aircraft Organization
[Legal Notices]    [Privacy Policy]