Boeing 767: Difference between revisions

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==767-400ER==
==767-400ER==
==Specifications==
==Specifications==
Powerplants
==Specifications==
Two 213.5kN (48,000lb) Pratt & Whitney JT9D-7R4 turbofans or 222.4kN (50,000lb) JT9D-7R4Es, or 222.4kN (50,000lb) PW-4050, or 233.5kN (52,000lb) PW-4052s, or 213.5kN (48,000lb) General Electric CF6-80As or 213.5kN (48,000lb) CF6-80A2s, or 231.3kN (52,500lb) CF6-80C2B2s, or 257.5kN (57,900lb) CF6-80C2B4Fs, or 269.9kN (60,000lb) RollsRoyce RB-211-524Gs.
{| class=wikitable style="text-align: center; font-size:100%; color:black"
767-300ER - Same options or 252.4kN (56,750lb) PW-4056s or 266.9kN (60,000lb) CF6-80C2B6s, or two PW-4060 rated at 60,000 lbs MTO
|-
 
!
Performance
! 767-200
Max cruising speed 900km/h (486kt), economical cruising speed 850km/h (460kt). Higher gross weight version range with design payload and PW-4050s 7835km (4230nm), with CF6-80C2B2s 7890km (4260nm).
! 767-200ER
767-300ER - Range with design payload with PW-4060s 10,880km (5875nm), with CF6-80C2B4Fs 10,195km (5505nm).
! 767-300
 
! 767-300ER
Weights
! 767-300F
767-300 - Empty with PW-4050s 79,560kg (175,400lb), with CF6-80C2B2s 79,379kg (175,000lb). Operating empty with PW-4050s 87,135kg (192,100lb), with CF6-80C2B2s 86,955kg (191,700lb). Higher gross weight version max takeoff with PW-4050s or CF6-80C2B2s 159,210kg (351,000lb).
! 767-400ER
767-300ER - Empty with PW-4060s 81,374kg (179,400lb), with CF6-80C2B4s 80,603kg (177,700lb). Operating empty with PW-4060s 90,535kg (199,600lb), with CF6-80C2B4s 90,175kg (198,800lb). Max takeoff with PW-4060s 181,890kg (401,000lb), with CF6-80C2B4Fs 175,540kg (387,000lb).
|-
 
!Cockpit crew
Dimensions
| colspan="6" | Two
Wing span 47.57m (156ft 1in), length 54.94m (180ft 3in), height 15.85m (52ft 0in). Wing area 283.3m2 (3050sq ft).
|-
 
! Passengers
Capacity
| colspan="2" | 181 (3 class) <br/> 224 (2 class) <br/> 255 optional 290 (1 class)
Flightcrew of two. Typical three class layout for 210, two class 269 (24 premium & 245 economy seven abreast) max seating for 350 at eight abreast. Underfloor capacity for 20 LD2s.
| colspan="2" | 218 (3 class) <br/> 269 (2 class) <br/> 350 (1 class)
 
| -
Production
| 245 (3 class) <br/> 304 (2 class) <br/> 375 (1 class)
565 767-300s (including ERs) had been ordered by late 1998, of which 496 had been delivered.
|-
! Cargo
| colspan="2" | 2,875&nbsp;ft³ (81.4 m³)<br>22 LD2s
| colspan="2" | 3,770&nbsp;ft³ (106.8 m³)<br>30 LD2s
| 16,034&nbsp;ft³ (454&nbsp;m³)<br>30&nbsp;LD2s + 24&nbsp;pallets
| 4,580&nbsp;ft³ (129.6&nbsp;m³)<br>38&nbsp;LD2s
|-
! Length
| colspan="2" | 159&nbsp;ft 2 in<br/>(48.5&nbsp;m)
| colspan="3" | 180&nbsp;ft 3 in<br/>(54.9&nbsp;m)
| 201&nbsp;ft 4 in<br/>(61.4&nbsp;m)
|-
! Wingspan
| colspan="5" | 156&nbsp;ft 1 in<br/>(47.6&nbsp;m)
| 170&nbsp;ft 4 in<br/>(51.9&nbsp;m)
|-
! Wing area
|colspan="5" | 3,050&nbsp;ft² (283.3 sq m²)
| 3,130&nbsp;ft ² (290.7 m²)
|-
!Fuselage height
|colspan="6"|17&nbsp;ft 9&nbsp;in (5.41&nbsp;m)
|-
!Fuselage width
|colspan="6"|16&nbsp;ft 6 in (5.03&nbsp;m)
|-
!Cabin width (interior)
|colspan="6"|15&nbsp;ft 6 in (4.72&nbsp;m)
|-
! Empty Weight, <br/>operating
| 176,650 lb <br> (80,130&nbsp;kg)  
| 181,610&nbsp;lb <br> (82,380&nbsp;kg)
| 189,750&nbsp;lb <br> (86,070&nbsp;kg)
| 198,440&nbsp;lb <br> (90,010&nbsp;kg)
| 190,000&nbsp;lb <br> (86,180&nbsp;kg)
| 229,000&nbsp;lb <br> (103,870&nbsp;kg)
|-
! Maximum take-off weight
| 315,000&nbsp;lb <br> (142,880&nbsp;kg)  
| 395,000&nbsp;lb <br> (179,170&nbsp;kg)
| 350,000&nbsp;lb <br> (158,760&nbsp;kg)
| 412,000&nbsp;lb <br> (186,880&nbsp;kg)
| 412,000&nbsp;lb <br> (186,880&nbsp;kg)
| 450,000&nbsp;lb <br> (204,120&nbsp;kg)
|-
! Maximum Range <br/>at MTOW
| 3,950 NM<br/>(7,300&nbsp;km)<br/>transatlantic
| 6,590 NM<br/>(12,200&nbsp;km)<br/>transpacific
| 3,950 NM<br/>(7,300&nbsp;km)<br/>transatlantic
| 5,975 NM<br/>(11,065&nbsp;km)<br/>transpacific
| 3,255 NM<br/>(6,025&nbsp;km)<br/>transcontinental
| 5,625 NM<br/>(10,415&nbsp;km)<br/>transpacific
|-
! Cruise speed
| colspan="6" | Mach 0.80 (470 kn, 530&nbsp;mph, 851&nbsp;km/h at 35,000&nbsp;ft cruise altitude)
|-
! Max. Cruise speed
| colspan="6" | Mach 0.86 (493 kn, 568&nbsp;mph, 913&nbsp;km/h at 35,000&nbsp;ft cruise altitude)
|-
! Takeoff run<br>at MTOW
| colspan=2 | 5,600&nbsp;ft (1,710 m)  
| colspan=3 | 7,900&nbsp;ft (2,410 m)  
| 9,501&nbsp;ft (2,896 m)
|-
! Engines (x2)
| P&W JT9D-7R4 <br> P&W PW4000-94 <br> GE CF6-80A <br> GE CF6-80C2
| P&W PW4000-94 <br> GE CF6-80C2
| P&W JT9D-7R4<br> P&W PW4000-94 <br> GE CF6-80A <br>GE CF6-80C2
| colspan=2 | P&W PW4000-94 <br> GE CF6-80C2 <br> RR RB211-524H
| P&W PW4000-94 <br> GE CF6-80C2
|-
! Thrust (x2)
| GE: 50,000 lbf (222&nbsp;kN)
| PW: 63,300&nbsp;lb (282&nbsp;kN) <br> GE: 62,100&nbsp;lbf (276&nbsp;kN)
| PW: 50,000&nbsp;lbf (220&nbsp;kN)
| colspan=2 | PW: 63,300&nbsp;lbf (282&nbsp;kN) <br> GE: 62,100&nbsp;lbf (276&nbsp;kN) <br> RR: 59,500&nbsp;lbf (265&nbsp;kN)
| PW: 63,300&nbsp;lbf (282&nbsp;kN) <br> GE: 63,500&nbsp;lbf (282&nbsp;kN)
|}


[[Category:Widebody Jetliners]]
[[Category:Widebody Jetliners]]

Revision as of 03:17, 10 September 2009

Boeing 767 at a Glance
Role Widebody Jetliner
Country of Origin United States
Manufacturer Boeing
Status In Production
Number Built 977
Unit Cost 80,000,000-139,000,000
File:Airplanes-Boeing 767.jpg


767-200

767-200ER

767-200ERF

767-300

767-300ER

767-300F

767-400ER

Specifications

Specifications

767-200 767-200ER 767-300 767-300ER 767-300F 767-400ER
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 sq 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)
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 NM
(7,300 km)
transatlantic 		6,590 NM
(12,200 km)
transpacific 		3,950 NM
(7,300 km)
transatlantic 		5,975 NM
(11,065 km)
transpacific 		3,255 NM
(6,025 km)
transcontinental 		5,625 NM
(10,415 km)
transpacific
Cruise speed Mach 0.80 (470 kn, 530 mph, 851 km/h at 35,000 ft cruise altitude)
Max. Cruise speed Mach 0.86 (493 kn, 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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