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  2. Changhe Z-10 - Wikipedia

    en.wikipedia.org/wiki/Changhe_Z-10

    The Changhe Z-10 (Chinese: 直-10; pinyin: Zhí-Shí; lit. 'helicopter-10') is a Chinese medium-weight, twin-turboshaft attack helicopter built by the Changhe Aircraft Industries Corporation for the People's Liberation Army Ground Force.

  3. Changhe Aircraft Industries Corporation - Wikipedia

    en.wikipedia.org/wiki/Changhe_Aircraft...

    Changhe employs 4300 employees in two production facilities with 1.29 million sq. metres and 0.22 million sq. metres of construction area. It has a joint venture with Agusta Helicopter (Jiangxi Changhe-Agusta Helicopter Co., Ltd) and relationship with Sikorsky Aircraft Corporation. [3]

  4. People's Liberation Army Ground Force Aviation - Wikipedia

    en.wikipedia.org/wiki/People's_Liberation_Army...

    This accelerated program would lead to the introduction in 1994 of the Harbin Z-9 (developed from the French Eurocopter AS365 Dauphin), the Harbin Z-19 (an armed variant of the Z-9, introduced in 2012), the medium attack Changhe Z-10 (introduced in 2012), and the medium utility helicopter Harbin Z-20 (generally based on the Black Hawk in ...

  5. China's Z-10 attack helicopter makes foreign debut, but ... - AOL

    www.aol.com/news/chinas-z-10-attack-helicopter...

    China's AVIC displayed its Z-10 attack helicopter for the first time outside its home country at the Singapore Airshow - the only non-Western design on display in a year in which no Russian ...

  6. Z10 - Wikipedia

    en.wikipedia.org/wiki/Z10

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Help; Learn to edit; Community portal; Recent changes; Upload file

  7. Changhe Z-11 - Wikipedia

    en.wikipedia.org/wiki/Changhe_Z-11

    Data from Jane's All The World's Aircraft 2010–2011 General characteristics Crew: 1 Capacity: 3 (reconnaissance variants) 6 (utility variants) Length: 11.24 m (36 ft 11 in) fuselage 13.01 m (43 ft) with rotors turning Width: 1.8 m (5 ft 11 in) Height: 3.14 m (10 ft 4 in) to top of rotor hub Empty weight: 1,253 kg (2,762 lb) Max takeoff weight: 2,250 kg (4,960 lb) Fuel capacity: 423 kg (933 ...

  8. Aeronautical chart - Wikipedia

    en.wikipedia.org/wiki/Aeronautical_chart

    An aeronautical chart is a map designed to assist in the navigation of aircraft, much as nautical charts do for watercraft, or a roadmap does for drivers. Using these charts and other tools, pilots are able to determine their position, safe altitude, best route to a destination, navigation aids along the way, alternative landing areas in case of an in-flight emergency, and other useful ...

  9. Marine Corps confirms the worst: All 5 troops killed in ... - AOL

    www.aol.com/news/know-search-five-marines...

    The helicopter carrying five Marines that crashed during a storm in the mountains outside San Diego was a CH-53E Super Stallion designed to fly through bad weather, even at night. The Super ...