Flat Wing Aspect Ratio
7.99
Cruise Speed
850.0673 km/h
Entry Into service
1982-09-08
Maximum Take-Off Weight
186.88 t (paragliders: kg)
Total Fuel Capacity
91380
Maximum Range
10667.52 km
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
767-200 |
186.88 |
91380 |
10667.52 |
Similar airplanes
All data (27 fields)
- Name
- 767-200
- Manufacturer
- Boeing
- Description
- The Boeing 767 is an American wide-body airliner developed and manufactured by Boeing Commercial Airplanes.
- ICAO Code
- B762
- EASA TCDSN
- EASA.IM.A.035
- First Flight
- 1981-09-26
- Entry Into service
- 1982-09-08
- Length (m)
- 54.94
- Height (m)
- 16.03
- Cockpit Crew
- 2
- Max Speed (km/h)
- 666.7194
- Cruise Speed (km/h)
- 850.0673
- Max Ceiling (m)
- 13136.88
- Capacity Description
- 290 (all economy), 299 (all economy with extra exit doors), or 261 (two classes) passengers, 4,030 cu ft (114.1 m3) of cargo (including 30 LD2 containers)
- Max Mach (Mach)
- 0.86
- National Origin
- United States of America
- Number Built
- 1373
- Powerplant Description
- 2 × Pratt & Whitney PW4060 high-bypass turbofan engines, 27216 kN thrust each
- Primary Users
- Delta Air Lines, FedEx Express, UPS Airlines, United Airlines
- Status
- In service; cargo and military variants in production
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Boeing_767
- Flat Wing Span (m)
- 47.57
- Flat Wing Area (m²)
- 283.3
- Flat Wing Aspect Ratio
- 7.99
- Wake Category
- H
- Aircraft Engine
- Pratt & Whitney PW4000
- Number of Engines
- 2