Dragon Wings – Boeing C-17 Globemaster III , 62nd Airlift Wing Air Mobility Command McChord AFB

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                         Boeing C-17 Globemaster III

Boeing (dříve McDonnell Douglas) C-17 Globemaster III je strategický transportní letoun vyráběný společností Boeing Integrated Defense Systems, a sloužící v letectvech USA, Británie, Austrálie, Kanady, Indie, Kataru a Spojených arabských emirátů.

The Boeing C-17 Globemaster III is a large military transport aircraft. It was developed for the United States Air Force (USAF) from the 1980s to the early 1990s by McDonnell Douglas.

Role Strategic and tactical airlifter
National origin United States
Manufacturer McDonnell Douglas / Boeing
First flight 15 September 1991
Introduction 17 January 1995
Status In service
Primary users United States Air Force
Indian Air Force
Royal Air Force
See Operators for others
Produced 1991–2015
Number built 279
Unit cost
US$218 million (flyaway cost for FY 2007)
Developed from McDonnell Douglas YC-15

The C-17 carries forward the name of two previous piston-engined military cargo aircraft, the Douglas C-74 Globemaster and the Douglas C-124 Globemaster II. The C-17 commonly performs tactical and strategic airlift missions, transporting troops and cargo throughout the world; additional roles include medical evacuation and airdrop duties. It was designed to replace the Lockheed C-141 Starlifter, and also fulfill some of the duties of the Lockheed C-5 Galaxy, freeing the C-5 fleet for outsize cargo.

General characteristics

  • Crew: 3: 2 pilots, 1 loadmaster
  • Capacity:
    • 102 paratroopers or
    • 134 troops with palletized and sidewall seats or
    • 54 troops with sidewall seats (allows 13 cargo pallets) only or
    • 36 litter and 54 ambulatory patients and medical attendants or
    • Cargo, such as one M1 Abrams tank, three Strykers, or six M1117 Armored Security Vehicles
  • Payload: 170,900 lb (77,520 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles
  • Length: 174 ft (53 m)
  • Wingspan: 169.8 ft (51.75 m)
  • Height: 55.1 ft (16.8 m)
  • Wing area: 3,800 ft² (353 m²)
  • Empty weight: 282,500 lb (128,100 kg)
  • Max. takeoff weight: 585,000 lb (265,350 kg)
  • Fuel capacity: 35,546 U.S. gal (134,556 L)
  • Powerplant: 4 × Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each

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