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A Boeing CH-47 Chinook at Campbell Army Airfield on 7 August 2012 delivering two Humvees by sling load. On 6 August 2011, a Chinook crashed near Kabul, killing all of the 38 aboard. The Chinook was reportedly shot down with a rocket-propelled grenade by the Taliban while attempting to assist a group of U.S. Navy SEALs. The 38 were members of ...
July 27: A Dutch Army CH-47 Chinook helicopter rolled and crashed during a night mission in Afghanistan. [189] June 28: A US CH-47 Chinook helicopter was shot down in Kunar province by Taliban commander Qari Ismail, killing all sixteen US Special Operations servicemen on board. The US military said it was shot down by a rocket-propelled grenade.
Pages in category "Boeing CH-47" ... Boeing CH-47 Chinook; B. Boeing CH-47 Chinook in Australian service; Boeing Chinook (UK variants) Boeing Vertol BV-347; Bravo ...
This category includes accidents and incidents involving the Boeing CH-47 Chinook and variants e.g. Boeing Chinook (UK variants) Pages in category "Accidents and incidents involving the Boeing Chinook"
Boeing Vertol CH-47 Chinook. Boeing Rotorcraft Systems (formerly Boeing Helicopters and before that Boeing Vertol) is the former name of an American aircraft manufacturer, now known as Vertical Lift division of Boeing Defense, Space & Security. The headquarters and main rotorcraft factory is in Ridley Park, Pennsylvania, a suburb of Philadelphia.
July 14, 1977: A U.S. Army CH-47 Chinook helicopter is shot down after straying into the north over the DMZ. Three airmen are killed and one is briefly held prisoner (this was the sixth such incident since the armistice was signed).
The 1978 Iranian Chinook shootdown was an incident on 21 June 1978, when four Boeing CH-47 Chinooks of the Imperial Iranian Air Force strayed into Soviet airspace during a training mission, with the result being that two of them were shot down by the PVO.
Tandem-rotor craft (such as in the Boeing CH-47 Chinook) also employ two rotors spinning in opposite directions—termed counter-rotation when it occurs from two separate points on the same airframe—but have the rotors on separate drive shafts through masts at the nose and tail. This configuration uses differential collective pitch to change ...
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