Boeing 767 Profile

Boeing 767 Profile

The Boeing 767 is an airliner produced by Boeing Commercial Airplanes which have mid-size wide-body twin-engine. The 767 was also the first Boeing wide-body airliner with a two-person flight deck, eliminating the need for a flight engineer.

Role : Wide-body jet airliner
National origin : United States
Manufacturer : Boeing Commercial Airplanes
First flight : September 26, 1981
Introduced : September 8, 1982 with United Airlines
Status : In production
Primary users : Delta Air Lines, American Airlines, All Nippon Airways, Japan Airlines
Produced : 1982–present
Unit cost :
-767-200ER: US$144.1 million
-767-300ER: US$164.3 million
-767-300F: US$167.7 million
-767-400ER: US$180.6 million
Variants : Boeing E-767, Boeing KC-46, Boeing KC-767,Northrop Grumman E-10 MC2A

The

Boeing 767

incorporated technological advances in avionics, engines, and wing design.The Boeing 767 is a low-wing cantilever monoplane with a conventional tail unit with a single fin and rudder.

The original Boeing 767 cockpit design, shared with the 757, uses six Rockwell Collins cathode ray tube (CRT) screens to display electronic flight instrumentation. There are three basic variants of the 767; The 767-200 was the original variant launched in 1978, followed by the 767-300 in 1982, and the 767-400ER in 1997.

Boeing 767 Specifications

767-200 767-200ER 767-300 767-300ER 767-300F 767-400ER
Cockpit crew Two
Seating capacity,
typical
181 (3-class)
224 (2-class)
255; optional 290 (1-class)
218 (3-class)
269 (2-class)
350 (1-class)
N/A 245 (3-class)
304 (2-class)
375 (1-class)
Boeing 767 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
Boeing 767 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
16,700 US gal (63,000 L) 24,100 US gal (91,000 L) 16,700 US gal (63,000 L) 24,100 US gal (91,000 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
takeoff 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 (11,000 m) cruise altitude)
Max. Cruise
speed
Mach 0.86 (493 knots, 568 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
Takeoff distance
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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