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The Boeing 767 is a mid-size, wide-body twinjet airliner produced by Boeing Commercial Airplanes. Passenger versions of the 767 can carry between 181 and 375 passengers, and have a range of 5,200 to 6,590 nautical miles (9,400 to 12,200 km) depending on variant and seating configuration. The Boeing 767 has been produced in three fuselage lengths. The original 767-200 first entered into airline service in 1982, followed by the 767-300 in 1986, and the 767-400ER in 2000. Extended range versions of the original -200 and -300 models, the 767-200ER and 767-300ER, have been produced with added payload and operating distance capability. The 767-300F, a freighter version, entered service in 1995.
The first wide-body twinjet produced by Boeing, the 767 was conceived and designed in tandem with the narrow-body Boeing 757 twinjet. Both airliners share design features and flight decks, enabling pilots to obtain a common type rating to operate the two aircraft. The 767 was the first Boeing wide-body airliner to enter service with a two-person crew flight deck, eliminating the need for a flight engineer. Following in-service indications of its twinjet design reliability, the 767 received regulatory approval allowing extended transoceanic operations beginning in 1985.
Through the 1990s, the Boeing 767 became commonly used on medium long-haul routes, and the aircraft has ranked as the most commonly used airliner for transatlantic flights between the United States and Europe. There have been over 1,000 Boeing 767s ordered with over 900 delivered as of 2010.[ ]
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| Orders and deliveries : E-10 |
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767-200 |
767-200ER |
767-300 |
767-300ER |
767-300F |
767-400ER |
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| Cockpit crew |
Two |
| Passengers |
181 (3 class)
224 (2 class)
255 optional 290 (1 class) |
218 (3 class)
269 (2 class)
350 (1 class) |
245 (3 class)
304 (2 class)
375 (1 class) |
| Cargo |
2,875 ft³ (81.4 m³)
22 LD2s |
3,770 ft³ (106.8 m³)
30 LD2s |
16,034 ft³ (454 m³)
30 LD2s + 24 pallets |
4,580 ft³ (129.6 m³)
38 LD2s |
| Length |
159 ft 2 in
(48.5 m) |
180 ft 3 in
(54.9 m) |
201 ft 4 in
(61.4 m) |
| Wingspan |
156 ft 1 in
(47.6 m) |
170 ft 4 in
(51.9 m) |
| Wing area |
3,050 ft2 (283.3 m2) |
3,130 ft 2 (290.7 m2) |
| Fuselage height |
17 ft 9 in (5.41 m) |
| Fuselage width |
16 ft 6 in (5.03 m) |
| Cabin width (interior) |
15 ft 6 in (4.72 m) |
| Maximum Fuel Capacity |
23,980 U.S. gal (90,770 L) |
Empty Weight,
operating |
176,650 lb
(80,130 kg) |
181,610 lb
(82,380 kg) |
189,750 lb
(86,070 kg) |
198,440 lb
(90,010 kg) |
190,000 lb
(86,180 kg) |
229,000 lb
(103,870 kg) |
| Maximum take-off weight |
315,000 lb
(142,880 kg) |
395,000 lb
(179,170 kg) |
350,000 lb
(158,760 kg) |
412,000 lb
(186,880 kg) |
412,000 lb
(186,880 kg) |
450,000 lb
(204,120 kg) |
Maximum Range
at MTOW |
3,950 nmi
(7,300 km)
transatlantic |
6,590 nmi
(12,200 km)
transpacific |
3,950 nmi
(7,300 km)
transatlantic |
5,975 nmi
(11,065 km)
transpacific |
3,255 nmi
(6,025 km)
transcontinental |
5,625 nmi
(10,415 km)
transpacific |
| Cruise speed |
Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft cruise altitude) |
| Max. Cruise speed |
Mach 0.86 (493 knots, 568 mph, 913 km/h at 35,000 ft cruise altitude) |
Takeoff run
at MTOW |
5,600 ft (1,710 m) |
7,900 ft (2,410 m) |
9,501 ft (2,896 m) |
| Engines (x2) |
P&W JT9D-7R4
P&W PW4000-94
GE CF6-80A
GE CF6-80C2 |
P&W PW4000-94
GE CF6-80C2 |
P&W JT9D-7R4
P&W PW4000-94
GE CF6-80A
GE CF6-80C2 |
P&W PW4000-94
GE CF6-80C2
RR RB211-524H |
P&W PW4000-94
GE CF6-80C2 |
| Thrust (x2) |
GE: 50,000 lbf (222 kN) |
PW: 63,300 lb (282 kN)
GE: 62,100 lbf (276 kN) |
PW: 50,000 lbf (220 kN) |
PW: 63,300 lbf (282 kN)
GE: 62,100 lbf (276 kN)
RR: 59,500 lbf (265 kN) |
PW: 63,300 lbf (282 kN)
GE: 63,500 lbf (282 kN) |
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