Developing nation: |
United States of America |
Manufacturer/designer: |
Boeing Commercial Airplane Company. |
Production line: |
Everett, WA. |
Type aircraft: |
Medium to long range widebody airliner. |
First flight: |
– 767-200 September 26, 1981 N767BA.- 767-200ER March 6, 1984.- 767-300 January 30, 1986 N767S.
– 767-300ER December 9, 1986.
– 767-300F June 20, 1995.
– 767-400ER October 9, 1999 N76700. |
First delivery: |
– 767-200 August 19, 1982 to United Airlines.- 767-200ER March 26, 1984 to El Al.- 767-300 September 25, 1986 to Japan Air Lines.
– 767-300ER February 19, 1988 to American Airlines.
– 767-300F October 12, 1995 to United Parcel Service.
– 767-400ER August 29, 2000 to Continental Airlines. |
|
Boeing 767-200 |
Cockpit crew: |
Two pilots. |
Passengers single class: |
245. |
Passengers two class: |
– 18 first class.- 198 economy class. |
Passengers three class: |
– 15 first class.- 40 business class.- 119 economy class. |
Cabin length: |
33,93 m. |
Cabin diameter: |
4,72 m. |
Cabin height: |
2,87 m. |
Cabin floor area: |
154,9 m². |
Cabin volume: |
428,2 m³. |
Baggage compartment: |
12,2 m³. |
Cargo volume: |
– main deck 428,2 m³.- under floor 74,8 m³.- baggage compartment 12,2 m³.
– total load 512,2 m³. |
LD2 containers in belly: |
22. |
Standard 2.24m x 3.17m pallets: |
– in belly 3 with 10 LD2 containers. |
Wing span: |
47,57 m. |
Wing area: |
283,35 m². |
Wing sweep: |
31,5 degrees. |
Fuselage length: |
48,51 m. |
Fuselage diameter: |
5,03 m. |
Height: |
15,85 m. |
Horizontal tail unit: |
18,62 m. |
Wheelbase: |
19,69 m. |
Track: |
9,30 m. |
Engines: |
– two Pratt & Whitney JT9D-7R4D each rated 213.5 kN.- two Pratt & Whitney JT9D-7R4E each rated 222.4 kN.- two Pratt & Whitney PW4052 each rated 231.3 kN.
– two General Electric CF6-80A each rated 208.8 kN.
– two General Electric CF6-80A2 each rated 216.5 kN.
– two General Electric CF6-80C2-B2 each rated 231.1 kN. |
Weight: |
– empty: 80.377 Kg.- max. zero-fuel weight: 113.398 Kg.- fuel: 63.216 liter.
– max. payload: 32.568 Kg. |
Max. take off weight: |
142.881 Kg. |
Max. landing weight: |
123.377 Kg. |
Cruise speed: |
852 km/h. |
Max. speed: |
898 km/h. |
Max. ceiling: |
11.887 m. |
Range: |
– max. range 12.235 km. |
Performance: |
– take-off run 1.707 m at max. take-off weight. |
|
Boeing 767-200ER* |
Engines: |
– two Pratt & Whitney PW4056 each rated 252.4 kN.- two General Electric CF6-80C2B4F each rated 254.79 kN.- two Rolls Royce RB211-524G each rated 253 kN.
– two Rolls Royce RB211-524H each rated 264.4 kN. |
Weight: |
– empty: 84.822 Kg.- max. zero-fuel weight: 117.934 Kg.- fuel: 91.380 liter.
– max. payload: 35.607 Kg. |
Max. take off weight: |
179.169 Kg. |
Max. landing weight: |
136.078 Kg. |
Cruise speed: |
852 km/h. |
Max. speed: |
896 km/h. |
Max. ceiling: |
11.887 m. |
Range: |
– max. range 12.316 km. |
Performance: |
– take-off run 1.707 m at max. take-off weight. |
* Generally similar to the Boeing 767-200 except in the following particulars.
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