Technical Specifications
Crew
2/6
Passengers
22 B 224 E, max. 246
Propulsion
2 Turbofan Engines
Engine Model
Pratt & Whitney PW4062
Engine Power (each)
275,8 kN
62000 lbf
Speed
850 km/h
459 kts
528 mph
Mmo (max. Mach)
Mach 0.80
Service Ceiling
13.137 m
43.100 ft
Range
11.066 km
5.975 NM
6.876 mi.
Empty Weight
88.469 kg
195.040 lbs
max. Takeoff Weight
181.437 kg
400.000 lbs
max. Landing Weight
145.150 kg
320.000 lbs
Wing Span
47,57 m
156 ft 1 in
Wing Area
283,3 m²
3049 ft²
Length
54,90 m
180 ft 1 in
Height
16,80 m
55 ft 1 in
Production Status
in production
Production Range
1986-2024
Boeing
767-3
HISTORY
The Boeing 767 is a mid to large-size, long-range, wide-body twin-engine jet airliner built by Boeing commercial Airplanes, It was the manufacturer’s first wide-body twin-jet and its first airliner with a two-crew glass cockpit.
The aircraft has two turbofan engines, a conventional tail, and, for reduced aerodynamic drag, a supercritical wing design.
Designed as a smaller wide-body airliner than earlier aircraft such as the 747, the 767 has seating capacity for 181 to 375 persons and a design range of 3,850 to 6,385 nautical miles (7,130 to 11,825 km), depending on variant.
Development of the 767 occurred in tandem with a narrow-body twin-jet, the 757, resulting in shared design features which allow pilots to obtain a common type rating to operate both aircraft.