Boeing C-17 Globemaster III
Flat Wing Area
353.0316 m²
Flat Wing Aspect Ratio
7.165
Cruise Speed
833.3993 km/h
Entry Into service
1995-01-17
Maximum Take-Off Weight
265.3515 t (paragliders: kg)
Total Fuel Capacity
134556.2
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Boeing C-17 Globemaster III |
265.3515 |
134556.2 |
4481.84 |
Similar airplanes
All data (25 fields)
- Name
- Boeing C-17 Globemaster III
- Manufacturer
- Boeing
- Description
- The McDonnell Douglas/Boeing C-17 Globemaster III is a large military transport aircraft developed for the United States Air Force (USAF) during the 1980s and the early 1990s by McDonnell Douglas.
- First Flight
- 1991-09-15
- Entry Into service
- 1995-01-17
- Production End
- 2015-01-01
- Designer
- Boeing
- Length (m)
- 53.0352
- Height (m)
- 16.764
- Cockpit Crew
- 3
- Max Seating
- 102
- Cruise Speed (km/h)
- 833.3993
- Max Ceiling (m)
- 13716
- Capacity Description
- 170900 lb of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles; 102 paratroopers or; 134 troops with palletized and sidewall seats or; 54 troops with side…
- National Origin
- United States of America
- Number Built
- 279
- Powerplant Description
- 4 × Pratt & Whitney PW2000 turbofan engines
- Primary Users
- United States Air Force, Indian Air Force , Royal Air Force , Royal Australian Air Force
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Boeing_C-17_Globemaster_III
- Flat Wing Span (m)
- 51.5112
- Flat Wing Area (m²)
- 353.0316
- Flat Wing Aspect Ratio
- 7.165
- Aircraft Engine
- Pratt & Whitney PW2000
- Number of Engines
- 4