The 757 has the performance to serve short-, medium-, and

The 757 has the performance to serve short-, medium-, and

The 757 has the performance to serve
short-, medium-, and long-range missions
StartupBoeing
Two-class seating
250
757-300
Max
Basic
757-200
200
Max
Basic
The A321 does not
150
1
(2)
2
3
(4)
4
(6)
Range, 1,000 nmi (1,000 km)
Copyright © 2007 Boeing. All rights reserved.
5
(8)
General arrangement
StartupBoeing
757-200 and 757-300
38.0 m
(124 ft 10 in)
47.3 m
(155 ft 3 in)
54.4 m
(178 ft 7 in)
13.6 m
(44 ft 6 in)
7.3 m
(24 ft 0 in)
Copyright © 2007 Boeing. All rights reserved.
757-CO-2000 11/6/06 JW/GG
Interior arrangements
StartupBoeing
757-200/-300, inclusive-tour seating
757-200 (overwing exits)
221 economy at 30-in pitch
221 passengers
757-200 (four doors)
228 economy at 28-in pitch
228 passengers
757-300
280 economy at 28-in pitch
280 passengers
B570621
B570623a
B570607
Copyright © 2007 Boeing. All rights reserved.
757-AO-0250• 01-30-03-JW/GG
Interior arrangements
StartupBoeing
757-200/-300, two-class seating
757-200 (overwing exits)
12 first at 36-in pitch
188 economy at 32-in pitch
200 passengers
757-200 (four doors)
12 first at 36-in pitch
182 economy at 32-in pitch
194 passengers
757-300
12 first at 36-in pitch
231 economy at 32-in pitch
243 passengers
B570505
B570507
B570606
Copyright © 2007 Boeing. All rights reserved.
757-AO-0251• 01-30-03-JW/GG
Door arrangements
StartupBoeing
757-200
Overwing exits
Four doors
Copyright © 2007 Boeing. All rights reserved.
757-DS-0006• 01-30-03-JW/GG
757 First Class Interior Seating
Copyright © 2007 Boeing. All rights reserved.
StartupBoeing
757 Economy Class Interior Seating
Copyright © 2007 Boeing. All rights reserved.
StartupBoeing
757 Interior Configurations
First class
StartupBoeing
Business class
Economy class
116.8
(46.0)
48.3
(19.0)
53.3
(21.0)
17.8
(7.0)
10.2
(4.0)
61.0
(24.0)
175.3
(69.0)
10.2
(4.0)
5.1
(2.0)
6.4
(2.5)
8.9
(3.5)
144.8
(57.0)
43.2
(17.0)
213.9
(84.2)
58.4
(23.0)
116.8
(46.0)
149.9
(59.0)
50.8
(20.0)
• Dimensions in centimeters (inches).
Copyright © 2007 Boeing. All rights reserved.
757-IN-2000 11.6.06 HW.GG
Cargo and baggage capability
StartupBoeing
757-200/-300
Vacuum waste system
DOOR
DOOR E6
Forward
Aft
Total volume
757-200
Bulk volume, m3 (ft3)
Load capability, kg (lb)
19.8 (699)
4,670 (10,300)
27.5 (971)
7,390 (16,300)
47.3 (1,670)
757-300
Bulk volume, m3 (ft3)
Load capability, kg (lb)
30.3 (1,071)
7,300 (16,100)
36.8 (1,299)
8,845 (19,500)
67.1 (2,370)
Copyright © 2007 Boeing. All rights reserved.
757-CA-2000 11/6/06 JW/GG
757-200 performance summary
StartupBoeing
Pratt & Whitney engines – Two Class
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m3 (ft3)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal )
nmi (km)
m (ft)
ft
m (ft)
kias
kg (lb)
kg (lb)
Maximum
200 (12/188)
47.3 (1,670)
PW2037
36,600/87
100,240 (221,000)
99,790 (220,000)
89,810 (198,000)
83,460 (184,000)
59,160 (130,440)
42,680 (11,276)
2,460 (4,550)
0.80
1,825 (6,000)
38,300
1,475 (4,850)
132
PW2040
40,100/87
116,120 (256,000)
115,660 (255,000)
95,250 (210,000)
84,360 (186,000)
59,160 (130,440)
43,490 (11,489)
3,915* (7,250)*
0.80
2,360 (7,750)
35,300
1,550 (5,100)
137
21.7 (47.8)
38.5 (84.9)
• Two-class seating.
• Typical mission rules.
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2000 11/6/06 JW/GG
757-200 performance summary
StartupBoeing
Rolls-Royce engines – Two Class
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m (ft)
Maximum
m (ft)
ft
m (ft)
kias
200 (12/188)
47.3 (1,670)
RB211-535E4
RB211-535E4B
40,200/84
43,500/77
100,240 (221,000)
116,120 (256,000)
99,790 (220,000)
115,660 (255,000)
89,810 (198,000)
95,250 (210,000)
83,460 (184,000)
84,360* (186,000)*
59,300 (130,730)
59,300 (130,730)
42,680 (11,276)
43,490 (11,489)
2,290 (4,240)
3,685** (6,825)**
0.80
0.80
1,660 (5,450)
2,070 (6,800)
38,700
35,600
1,420 (4,660)
1,505 (4,950)
132
137
kg (lb)
kg (lb)
22.9 (50.6)
40.6 (89.5)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
• Two-class seating.
• Typical mission rules.
* MZFW of 85,275 kg (188,000 lb) is available if MTW is reduced to 115,210 kg (254,000 lb).
** Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2001 11/7/06 JW/GG
757-300 performance summary
StartupBoeing
Pratt & Whitney engines – Two Class
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m3 (ft3)
Maximum
243 (12/231)
67.1 (2,370)
m (ft)
ft
m (ft)
kias
PW2040
40,100/87
109,310 (241,000)
108,860 (240,000)
101,600 (224,000)
95,250 (210,000)
64,470 (142,140)
43,400 (11,466)
2,105 (3,890)
0.80
2,100 (6,900)
36,950
1,735 (5,700)
142
PW2043
42,600/96
124,050 (273,500)
123,830 (273,000)
101,600 (224,000)
95,250 (210,000)
64,470 (142,140)
43,400 (11,466)
3,400* (6,295)*
0.80
2,635 (8,650)
34,250
1,735 (5,700)
142
kg (lb)
kg (lb)
19.8 (43.6)
35.7 (78.7)
19.8 (43.6)
35.7 (78.7)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
• Two-class seating.
• Typical mission rules.
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2002 11/7/06 JW/GG
757-300 performance summary
StartupBoeing
Rolls-Royce engines – Two Class
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m3 (ft3)
Maximum
m (ft)
ft
m (ft)
kias
243 (12/231)
67.1 (2,370)
RB211-535E4
RB211-535E4B
40,200/84
43,500/77
109,310 (241,000)
124,050 (273,500)
108,860 (240,000)
123,830 (273,000)
101,600 (224,000)
101,600 (224,000)
95,250 (210,000)
95,250 (210,000)
64,560 (142,340)
64,560 (142,340)
43,400 (11,466)
43,400 (11,466)
1,945 (3,600)
3,190* (5,910)*
0.80
0.80
2,115 (6,950)
2,605 (8,550)
36,950
34,300
1,735 (5,700)
1,735 (5,700)
142
142
kg (lb)
kg (lb)
20.9 (46.1)
37.8 (83.3)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
• Two-class seating.
• Typical mission rules.
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2003 11/7/06 JW/GG
757-200 performance summary
StartupBoeing
Pratt & Whitney engines - Inclusive Tour
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m3 (ft3)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
m (ft)
ft
m (ft)
kias
kg (lb)
kg (lb)
Maximum
228
47.3 (1,670)
PW2037
36,600/87
100,240 (221,000)
99,790 (220,000)
89,810 (198,000)
83,460 (184,000)
58,440 (128,840)
42,680 (11,276)
2,185 (4,045)
0.80
1,825 (6,000)
38,300
1,475 (4,850)
132
PW2040
40,100/87
116,120 (256,000)
115,660 (255,000)
95,250 (210,000)
84,360 (186,000)
58,440 (128,840)
43,490 (11,489)
3,845* (7,120)*
0.80
2,360 (7,750)
35,300
1,550 (5,100)
137
19.4 (42.7)
34.4 (75.7)
• Inclusive-tour seating.
• Typical mission rules.
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2004 11/7/06 JW/GG
757-200 performance summary
StartupBoeing
Rolls-Royce engines - Inclusive Tour
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m3 (ft3)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
m (ft)
ft
m (ft)
kias
kg (lb)
kg (lb)
Maximum
228
47.3 (1,670)
RB211-535E4
RB211-535E4B
40,200/84
43,500/77
100,240 (221,000)
116,120 (256,000)
99,790 (220,000)
115,660 (255,000)
89,810 (198,000)
95,250 (210,000)
83,460 (184,000)
84,360* (186,000)*
58,570 (129,130)
58,570 (129,130)
42,680 (11,276)
43,490 (11,489)
2,020 (3,740)
3,610** (6,685)**
0.80
0.80
1,660 (5,450)
2,070 (6,800)
38,700
35,600
1,420 (4,660)
1,505 (4,950)
132
137
20.5 (45.1)
36.3 (79.9)
20.5 (45.1)
36.3 (79.9)
• Inclusive-tour seating.
• Typical mission rules.
* MZFW of 85,275 kg (188,000 lb) is available if MTW is reduced to 115,210 kg (254,000 lb).
** Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2005 11/7/06 JW/GG
757-300 performance summary
StartupBoeing
Pratt & Whitney engines - Inclusive Tour
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
(FC/EC)
m3 (ft3)
Maximum
280
67.1 (2,370)
m (ft)
ft
m (ft)
kias
PW2040
40,100/87
109,310 (241,000)
108,860 (240,000)
101,600 (224,000)
95,250 (210,000)
64,340 (141,860)
43,400 (11,466)
1,680 (3,110)
0.80
2,100 (6,900)
36,950
1,735 (5,700)
142
PW2043
42,600/96
124,050 (273,500)
123,830 (273,000)
101,600 (224,000)
95,250 (210,000)
64,340 (141,860)
43,400 (11,466)
3,235* (5,990)*
0.80
2,635 (8,650)
34,250
1,735 (5,700)
142
kg (lb)
kg (lb)
17.6 (38.9)
32.0 (70.5)
17.6 (38.9)
31.9 (70.4)
lb/°F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
• Inclusive-tour seating.
• Typical mission rules.
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2006 11/7/06 JW/GG
757-300 performance summary
StartupBoeing
Rolls-Royce engines - Inclusive Tour
Basic
Passengers
Cargo volume
Engines
SL standard-day takeoff thrust/flat-rated temperature (BET)
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight
Fuel capacity
Design range (MTOW, full passenger payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW, ISA + 10°C)
Landing field length (MLW)
Approach speed (MLW)
Fuel burn/seat
500 nmi
1,000 nmi
Maximum
lb/°F
kg (lb)
kg (lb)
280
67.1 (2,370)
RB211-535E4
RB211-535E4B
40,200/87
43,500/77
109,310 (241,000)
124,055 (273,500)
108,860 (240,000)
123,830 (273,000)
kg (lb)
101,600 (224,000)
101,600 (224,000)
kg (lb)
kg (lb)
L (U.S. gal)
nmi (km)
95,250 (210,000)
64,430 (142,060)
43,400 (11,466)
1,540 (2,850)
0.80
2,115 (6,950)
36,950
1,735 (5,700)
142
95,250 (210,000)
64,430 (142,060)
43,400 (11,466)
3,020* (5,595)*
0.80
2,605 (8,550)
34,300
1,735 (5,700)
142
(FC/EC)
m3 (ft3)
m (ft)
ft
m (ft)
kias
kg (lb)
kg (lb)
18.7 (41.3)
33.8 (74.5)
• Inclusive-tour seating.
• Typical mission rules.
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-PS-2007 11/7/06 JW/GG
757-200/-300 payload-range capability
StartupBoeing
Payload, 1,000 kg (1,000 lb)
Pratt & Whitney engines – Two Class
40
(80)
(70)
757-300
108,860-kg (240,000-lb) MTOW
123,830-kg (273,000-lb) MTOW
35
30
757-200
(60)
(50)
(40)
99,790-kg (220,000-lb) MTOW
115,660-kg (255,000-lb) MTOW
25
20
15
(20)
10
(10)
5
(0)
0
200 passengers
y
c it
pa l )
ca ga 9)
el S. ,48
Fu (U. (11
L 0
,4 9
80
43
6
,
42 276)
,
(11
0
,40
43 466)
,
(11
(30)
243 passengers
0.0
0.5
(0)
• Two-class seating.
• Typical mission rules.
1.0
(2)
1.5
2.0
2.5
(4)
3.0
3.5
4.0
(6)
4.5
(8)
5.0
5.5
6.0
(10)
Range, 1,000 nmi (1,000 km)
Copyright © 2007 Boeing. All rights reserved.
757-PR-2000 11/7/06 JW/GG
757-200/-300 payload-range capability
Payload, 1,000 kg (1,000 lb)
StartupBoeing
Rolls-Royce engines – Two Class
40
(80)
(70)
(60)
(50)
(40)
757-300
108,860-kg (240,000-lb) MTOW
123,830-kg (273,000-lb) MTOW
35
30
757-200
99,790-kg (220,000-lb) MTOW
115,660-kg (255,000-lb)
MTOW
25
20
(10)
5
(0)
0
y
c it
pa l )
ca ga 9)
el S. ,48
Fu (U. 11
L 90 (
,4
10
43
(20)
200 passengers
0
,68
42 276)
,
(11
0
,40
43 466)
,
(11
(30)
15
243 passengers
0.0
0.5
(0)
• Two-class seating.
• Typical mission rules.
1.0
(2)
1.5
2.0
2.5
(4)
3.0
3.5
4.0
(6)
4.5
(8)
5.0
5.5
6.0
(10)
Range, 1,000 nmi (1,000 km)
Copyright © 2007 Boeing. All rights reserved.
757-PR-2001 11/7/06 JW/GG
757-200/-300 payload-range capability
StartupBoeing
Pratt & Whitney engines – Inclusive Tour
Payload, 1,000 kg (1,000 lb)
40
(80)
(70)
(60)
(50)
(40)
757-300
108,860-kg (240,000-lb) MTOW
123,830-kg (273,000-lb) MTOW
35
30
25
20
15
(20)
10
(10)
5
(0)
0
99,790-kg (220,000-lb) MTOW
115,660-kg (255,000-lb)
MTOW
280 passengers
228 passengers
y
c it
pa l )
ca ga 9)
el S. ,48
Fu (U. (11
L
0
,4 9
0
43
68
,
42 276)
,
(11
0
)
,40
43 ,466
(11
(30)
757-200
0.0
0.5
(0)
• Inclusive-tour seating.
• Typical mission rules.
1.0
(2)
1.5
2.0
2.5
(4)
3.0
3.5
4.0
(6)
4.5
(8)
5.0
5.5
6.0
(10)
Range, 1,000 nmi (1,000 km)
Copyright © 2007 Boeing. All rights reserved.
757-PR-2002 11/7/06 JW/GG
757-200/-300 payload-range capability
StartupBoeing
Rolls-Royce engines - Inclusive Tour
Payload, 1,000 kg (1,000 lb)
40
(80)
(70)
(60)
(50)
(40)
757-300
108,860-kg (240,000-lb) MTOW
123,830-kg (273,000-lb) MTOW
35
30
25
20
15
(20)
10
(10)
5
(0)
0
99,790-kg (220,000-lb) MTOW
115,660-kg (255,000-lb)
MTOW
280 passengers
228 passengers
y
c it
pa l )
ca ga 9)
el S. ,48
Fu (U. (11
L
0
,4 9
0
68
43
,
42 276)
,
(11
0
)
,40
43 ,466
(11
(30)
757-200
0.0
0.5
(0)
• Inclusive-tour seating.
• Typical mission rules.
1.0
(2)
1.5
2.0
2.5
(4)
3.0
3.5
4.0
(6)
4.5
(8)
5.0
5.5
6.0
(10)
Range, 1,000 nmi (1,000 km)
Copyright © 2007 Boeing. All rights reserved.
757-PR-2003 11/7/06 JW/GG
•
•
•
•
Long-range cruise
(LRC)
Still air range
Block time and fuel
Typical mission rules
Mission
Climb
5% mission
fuel allowance
Missed approach (VAPP to climb speed at 1,500 ft)
Taxi in (5 min) from reserves
Approach and land (5 min)
Decelerate to 250 kias
Descend to 1,500 ft
Descend to 10,000 ft
Climb
Climb to 1,500 ft; accel to 250 kias
Climb to 10,000 ft at 250 kias
Accelerate to climb speed
Takeoff (to 35 ft)
Taxi out (9 min)
LRC
100 nmi
Approach hold (30 min at 1,500 ft)
Approach and land (5 min)
Descend to 1,500 ft
Mission profile
StartupBoeing
Reserves
200 nmi
Typical reserves
Standard day.
Fuel density, 6.7 lb per U.S. gal.
Nominal performance.
Passengers at 90 kg (200 lb) passenger plus baggage.
Copyright © 2007 Boeing. All rights reserved.
757-AP-0387 02-14-03-TL/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Two Class
757-200
Warsaw
112,080-kg (247,100-lb) TOGW*
200 two-class passengers
Copenhagen
Anchorage
Paris
757-300
121,220-kg (267,240-lb) TOGW*
243 two-class passengers
Madrid
Seattle
Casablanca
Houston
NEW YORK
Bamako
Miami
Mexico City
Recife
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from New York.
Lima
La Paz
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2002 11/6/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Two Class
757-200
112,080-kg (247,100-lb) TOGW*
200 two-class passengers
Chicago
Novosibirsk
757-300
121,220-kg (267,240-lb) TOGW*
243 two-class passengers
Ottawa
New York
Islamabad
Karachi
LONDON
Muscat
Dakar
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from London.
Libreville
Nairobi
Luanda
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2001 11/6/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Two Class
757-200
Anchorage
112,080-kg (247,100-lb) TOGW*
200 two-class passengers
757-300
121,220-kg (267,240-lb) TOGW*
243 two-class passengers
Moscow
Baku
Karachi
BEIJING
Colombo
Jakarta
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from Beijing.
Darwin
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2000 11/6/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Two Class
757-200
112,080-kg (247,100-lb) TOGW*
200 two-class passengers
London
757-300
121,220-kg (267,240-lb) TOGW*
243 two-class passengers
Beijing
Madrid
Casablanca
Hong Kong
DUBAI
Accra
Singapore
Libreville
Jakarta
Luanda
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from Dubai.
Windhoek
Maputo
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2003 11/6/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Inclusive Tour
757-200
Warsaw
113,890-kg (251,100-lb) TOGW*
228 inclusive-tour passengers
Copenhagen
Anchorage
Paris
757-300
123,830-kg (273,000-lb) MTOW
280 inclusive-tour passengers
Madrid
Casablanca
Bamako
NEW YORK
Houston
Miami
Mexico City
Recife
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from New York.
Lima
La Paz
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2006 11/7/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Inclusive Tour
757-200
113,890-kg (251,100-lb) TOGW*
228 inclusive-tour passengers
Novosibirsk
757-300
123,830-kg (273,000-lb) MTOW
280 inclusive-tour passengers
Chicago
Ottawa
New York
Islamabad
Karachi
LONDON
Muscat
Dakar
Nairobi
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from London.
Libreville
Luanda
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2005 11/7/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Inclusive Tour
757-200
Anchorage
113,890-kg (251,100-lb) TOGW*
228 inclusive-tour passengers
Moscow
757-300
123,830-kg (273,000-lb) MTOW
280 inclusive-tour passengers
Baku
Karachi
BEIJING
Colombo
Jakarta
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from Beijing.
Darwin
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2004 11/7/06 JW/GG
The 757 is a transcontinental airplane
StartupBoeing
Full passenger payload - Inclusive Tour
757-200
113,890-kg (251,100-lb) TOGW*
228 inclusive-tour passengers
London
Madrid
Beijing
757-300
123,830-kg (273,000-lb) MTOW
280 inclusive-tour passengers
Casablanca
Hong Kong
DUBAI
Accra
Singapore
Libreville
Jakarta
Luanda
•
•
•
•
Typical mission rules.
85% annual winds.
Airways and traffic allowances included.
Range capability from Dubai.
Windhoek
Maputo
*Fuel volume limited.
Copyright © 2007 Boeing. All rights reserved.
757-CC-2007 11/7/06 JW/GG
757 Flight Deck
StartupBoeing
Copyright © 2007 Boeing. All rights reserved.
1/22/2008