boeing 757-200 - boeing: the boeing · pdf filestartupboeing • two-class seating. •...

Copyright © 2007 Boeing. All rights reserved.

StartupBoeing

Two-class seating

150

200

250

1 2 3 4 5

Max

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

757-200

Basic

Max

757-300

Basic

The A321 does not

Range, 1,000 nmi (1,000 km)(2) (4) (6) (8)


StartupBoeing

757-200 and 757-300

54.4 m(178 ft 7 in)

General arrangement

13.6 m(44 ft 6 in)

38.0 m(124 ft 10 in)

7.3 m(24 ft 0 in)

47.3 m(155 ft 3 in)

757-CO-2000 11/6/06 JW/GG


StartupBoeing

757-200/-300, inclusive-tour seating

Interior arrangements

280 passengers

228 passengers

221 passengers

757-300280 economy at 28-in pitch

757-200 (four doors)228 economy at 28-in pitch

757-200 (overwing exits)221 economy at 30-in pitch

B570621B570623aB570607

757-AO-0250• 01-30-03-JW/GG


StartupBoeing

757-200/-300, two-class seating

Interior arrangements

243 passengers

194 passengers

200 passengers

B570505B570507B570606

757-30012 first at 36-in pitch

231 economy at 32-in pitch

757-200 (four doors)12 first at 36-in pitch


757-200 (overwing exits)12 first at 36-in pitch


757-AO-0251• 01-30-03-JW/GG


StartupBoeingDoor arrangements

Overwing exits

Four doors

757-200

757-DS-0006• 01-30-03-JW/GG


StartupBoeing757 First Class Interior Seating


StartupBoeing757 Economy Class Interior Seating


StartupBoeing757 Interior Configurations

First class Business class Economy class

• Dimensions in centimeters (inches).

61.0(24.0)

144.8(57.0)

10.2(4.0)

53.3(21.0)

17.8(7.0)

58.4(23.0)

116.8(46.0)

6.4(2.5)

48.3(19.0)

8.9(3.5)

50.8(20.0)

149.9(59.0)

10.2(4.0)

43.2(17.0)

5.1(2.0)

175.3(69.0)

116.8(46.0)

213.9(84.2)

757-IN-2000 11.6.06 HW.GG


StartupBoeingCargo and baggage capability

DOOR DOOR E6

Vacuum waste system

Forward Aft Total volume

757-200Bulk 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)

757-300Bulk 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)

757-200/-300

757-CA-2000 11/6/06 JW/GG


StartupBoeing

• Two-class seating.• Typical mission rules.

*Fuel volume limited.

757-200 performance summaryPratt & Whitney engines – Two Class

Basic MaximumPassengers (FC/EC)

m3 (ft3)

lb/°Fkg (lb)kg (lb)kg (lb)kg (lb)kg (lb)

L (U.S. gal )nmi (km)

Cruise Mach 0.80 0.80Takeoff field length (SL, 86°F, MTOW) m (ft) 1,825 (6,000) 2,360 (7,750)Initial cruise altitude (MTOW, ISA + 10°C) ft 38,300 35,300Landing field length (MLW) m (ft) 1,475 (4,850) 1,550 (5,100)Approach speed (MLW) kias 132 137Fuel burn/seat

500 nmi kg (lb) 21.7 (47.8)1,000 nmi kg (lb) 38.5 (84.9)

200 (12/188)Cargo volume 47.3 (1,670)Engines PW2037 PW2040SL standard-day takeoff thrust/flat-rated temperature (BET) 36,600/87 40,100/87Maximum taxi weight 100,240 (221,000) 116,120 (256,000)Maximum takeoff weight 99,790 (220,000) 115,660 (255,000)Maximum landing weight 89,810 (198,000) 95,250 (210,000)Maximum zero fuel weight 83,460 (184,000) 84,360 (186,000)Operating empty weight 59,160 (130,440) 59,160 (130,440)Fuel capacity 42,680 (11,276) 43,490 (11,489)Design range (MTOW, full passenger payload) 2,460 (4,550) 3,915* (7,250)*

757-PS-2000 11/6/06 JW/GG


StartupBoeing


757-200 performance summary

Rolls-Royce engines – Two ClassBasic Maximum

Passengers (FC/EC)m (ft)


L (U.S. gal)nmi (km)


500 nmi kg (lb) 22.9 (50.6)1,000 nmi kg (lb) 40.6 (89.5)

200 (12/188)Cargo volume 47.3 (1,670)Engines RB211-535E4 RB211-535E4BSL standard-day takeoff thrust/flat-rated temperature (BET) 40,200/84 43,500/77Maximum taxi weight 100,240 (221,000) 116,120 (256,000)Maximum takeoff weight 99,790 (220,000) 115,660 (255,000)Maximum landing weight 89,810 (198,000) 95,250 (210,000)Maximum zero fuel weight 83,460 (184,000) 84,360* (186,000)*Operating empty weight 59,300 (130,730) 59,300 (130,730)Fuel capacity 42,680 (11,276) 43,490 (11,489)Design range (MTOW, full passenger payload) 2,290 (4,240) 3,685** (6,825)**

* MZFW of 85,275 kg (188,000 lb) is available if MTW is reduced to 115,210 kg (254,000 lb).** Fuel volume limited.

757-PS-2001 11/7/06 JW/GG


StartupBoeing757-300 performance summary

Pratt & Whitney engines – Two ClassBasic Maximum

Passengers (FC/EC)m3 (ft3)




500 nmi kg (lb) 19.8 (43.6) 19.8 (43.6)1,000 nmi kg (lb) 35.7 (78.7) 35.7 (78.7)

243 (12/231)Cargo volume 67.1 (2,370)Engines PW2040 PW2043SL standard-day takeoff thrust/flat-rated temperature (BET) 40,100/87 42,600/96Maximum taxi weight 109,310 (241,000) 124,050 (273,500)Maximum takeoff weight 108,860 (240,000) 123,830 (273,000)Maximum landing weight 101,600 (224,000) 101,600 (224,000)Maximum zero fuel weight 95,250 (210,000) 95,250 (210,000)Operating empty weight 64,470 (142,140) 64,470 (142,140)Fuel capacity 43,400 (11,466) 43,400 (11,466)Design range (MTOW, full passenger payload) 2,105 (3,890) 3,400* (6,295)*



757-PS-2002 11/7/06 JW/GG



Rolls-Royce engines – Two Class

Basic MaximumPassengers (FC/EC)

m3 (ft3)




500 nmi kg (lb) 20.9 (46.1)1,000 nmi kg (lb) 37.8 (83.3)

243 (12/231)Cargo volume 67.1 (2,370)Engines RB211-535E4 RB211-535E4BSL standard-day takeoff thrust/flat-rated temperature (BET) 40,200/84 43,500/77Maximum taxi weight 109,310 (241,000) 124,050 (273,500)Maximum takeoff weight 108,860 (240,000) 123,830 (273,000)Maximum landing weight 101,600 (224,000) 101,600 (224,000)Maximum zero fuel weight 95,250 (210,000) 95,250 (210,000)Operating empty weight 64,560 (142,340) 64,560 (142,340)Fuel capacity 43,400 (11,466) 43,400 (11,466)Design range (MTOW, full passenger payload) 1,945 (3,600) 3,190* (5,910)*



757-PS-2003 11/7/06 JW/GG



Pratt & Whitney engines - Inclusive TourBasic Maximum





500 nmi kg (lb) 19.4 (42.7)1,000 nmi kg (lb) 34.4 (75.7)

228Cargo volume 47.3 (1,670)Engines PW2037 PW2040SL standard-day takeoff thrust/flat-rated temperature (BET) 36,600/87 40,100/87Maximum taxi weight 100,240 (221,000) 116,120 (256,000)Maximum takeoff weight 99,790 (220,000) 115,660 (255,000)Maximum landing weight 89,810 (198,000) 95,250 (210,000)Maximum zero fuel weight 83,460 (184,000) 84,360 (186,000)Operating empty weight 58,440 (128,840) 58,440 (128,840)Fuel capacity 42,680 (11,276) 43,490 (11,489)Design range (MTOW, full passenger payload) 2,185 (4,045) 3,845* (7,120)*

• Inclusive-tour seating.• Typical mission rules.


757-PS-2004 11/7/06 JW/GG


StartupBoeing


* MZFW of 85,275 kg (188,000 lb) is available if MTW is reduced to 115,210 kg (254,000 lb).** Fuel volume limited.

757-200 performance summary

Rolls-Royce engines - Inclusive TourBasic Maximum





500 nmi kg (lb) 20.5 (45.1) 20.5 (45.1)1,000 nmi kg (lb) 36.3 (79.9) 36.3 (79.9)

228Cargo volume 47.3 (1,670)Engines RB211-535E4 RB211-535E4BSL standard-day takeoff thrust/flat-rated temperature (BET) 40,200/84 43,500/77Maximum taxi weight 100,240 (221,000) 116,120 (256,000)Maximum takeoff weight 99,790 (220,000) 115,660 (255,000)Maximum landing weight 89,810 (198,000) 95,250 (210,000)Maximum zero fuel weight 83,460 (184,000) 84,360* (186,000)*Operating empty weight 58,570 (129,130) 58,570 (129,130)Fuel capacity 42,680 (11,276) 43,490 (11,489)Design range (MTOW, full passenger payload) 2,020 (3,740) 3,610** (6,685)**

757-PS-2005 11/7/06 JW/GG



Pratt & Whitney engines - Inclusive TourBasic Maximum





500 nmi kg (lb) 17.6 (38.9) 17.6 (38.9)1,000 nmi kg (lb) 32.0 (70.5) 31.9 (70.4)

280Cargo volume 67.1 (2,370)Engines PW2040 PW2043SL standard-day takeoff thrust/flat-rated temperature (BET) 40,100/87 42,600/96Maximum taxi weight 109,310 (241,000) 124,050 (273,500)Maximum takeoff weight 108,860 (240,000) 123,830 (273,000)Maximum landing weight 101,600 (224,000) 101,600 (224,000)Maximum zero fuel weight 95,250 (210,000) 95,250 (210,000)Operating empty weight 64,340 (141,860) 64,340 (141,860)Fuel capacity 43,400 (11,466) 43,400 (11,466)Design range (MTOW, full passenger payload) 1,680 (3,110) 3,235* (5,990)*



757-PS-2006 11/7/06 JW/GG



Rolls-Royce engines - Inclusive TourBasic Maximum





500 nmi kg (lb) 18.7 (41.3)1,000 nmi kg (lb) 33.8 (74.5)

280Cargo volume 67.1 (2,370)Engines RB211-535E4 RB211-535E4BSL standard-day takeoff thrust/flat-rated temperature (BET) 40,200/87 43,500/77Maximum taxi weight 109,310 (241,000) 124,055 (273,500)Maximum takeoff weight 108,860 (240,000) 123,830 (273,000)Maximum landing weight 101,600 (224,000) 101,600 (224,000)Maximum zero fuel weight 95,250 (210,000) 95,250 (210,000)Operating empty weight 64,430 (142,060) 64,430 (142,060)Fuel capacity 43,400 (11,466) 43,400 (11,466)Design range (MTOW, full passenger payload) 1,540 (2,850) 3,020* (5,595)*



757-PS-2007 11/7/06 JW/GG


StartupBoeing

Payload, 1,000 kg (1,000 lb)

0

5

10

15

20

25

30

35

40

0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0

Range, 1,000 nmi (1,000 km)• Two-class seating.• Typical mission rules.

757-200/-300 payload-range capability

200 passengers

243 passengers

757-300108,860-kg (240,000-lb) MTOW123,830-kg (273,000-lb) MTOW


Fuel capacity

L (U.S. gal)

43,490 (11,489)

Pratt & Whitney engines – Two Class

757-PR-2000 11/7/06 JW/GG

43,400

(11,466)

42,680

(11,276)

(0) (2) (4) (6) (8) (10)

(0)

(10)

(20)

(30)

(40)

(50)

(60)

(70)

(80)


StartupBoeing

Payload, 1,000 kg (1,000 lb)

0

5

10

15

20

25

30

35

40

0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0

Range, 1,000 nmi (1,000 km)

Rolls-Royce engines – Two Class



200 passengers

243 passengers


757-20099,790-kg (220,000-lb) MTOW115,660-kg (255,000-lb)

MTOW

Fuel capacity

L (U.S. gal)

43,490 (11,489)

757-PR-2001 11/7/06 JW/GG

43,400

(11,466)

42,680

(11,276)

(0) (2) (4) (6) (8) (10)

(0)

(10)

(20)

(30)

(40)

(50)

(60)

(70)

(80)


StartupBoeing

Payload, 1,000 kg (1,000 lb)

0

5

10

15

20

25

30

35

40

0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0

Range, 1,000 nmi (1,000 km)

Pratt & Whitney engines – Inclusive Tour



228 passengers

280 passengers


757-20099,790-kg (220,000-lb) MTOW115,660-kg (255,000-lb)

MTOW

Fuel capacity

L (U.S. gal)

43,490 (11,489)

757-PR-2002 11/7/06 JW/GG

43,400

(11,466)

42,680

(11,276)

(0) (2) (4) (6) (8) (10)

(0)

(10)

(20)

(30)

(40)

(50)

(60)

(70)

(80)


StartupBoeing

Payload, 1,000 kg (1,000 lb)

0

5

10

15

20

25

30

35

40

0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0

Range, 1,000 nmi (1,000 km)

Rolls-Royce engines - Inclusive Tour



228 passengers

280 passengers


757-20099,790-kg (220,000-lb) MTOW115,660-kg (255,000-lb)

MTOW

Fuel capacity

L (U.S. gal)

43,490 (11,489)

757-PR-2003 11/7/06 JW/GG

43,400

(11,466)

42,680

(11,276)

(0) (2) (4) (6) (8) (10)

(0)

(10)

(20)

(30)

(40)

(50)

(60)

(70)

(80)


StartupBoeingMission profile

• Standard day.• Fuel density, 6.7 lb per U.S. gal.• Nominal performance.• Passengers at 90 kg (200 lb) passenger plus baggage.

Block time and fuel

Taxi

out

(9 m

in)

Typical reserves

200 nmi

Take

off (

to 3

5 ft)

Clim

b to

1,5

00 ft

; acc

elto

250

kia

sC

limb

to 1

0,00

0 ft

at 2

50 k

ias

Acc

eler

ate

to c

limb

spee

d

Clim

b

Des

cend

to 1

0,00

0 ft

Dec

eler

ate

to 2

50 k

ias

Des

cend

to 1

,500

ft

App

roac

h an

d la

nd (5

min

)

Taxi

in (5

min

) fro

m re

serv

es

Still air range

Long-range cruise (LRC)

5% m

issi

onfu

el a

llow

ance

Mis

sed

appr

oach

(VA

PPto

clim

b sp

eed

at 1

,500

ft)

Clim

bC

limb LRC

100 nmi

Des

cend

to 1

,500

ft

App

roac

h an

d la

nd (5

min

)

App

roac

h ho

ld (3

0 m

in a

t 1,5

00 ft

)

Mission ReservesTypical mission rules

757-AP-0387 02-14-03-TL/GG


StartupBoeingThe 757 is a transcontinental airplane

Full passenger payload - Two Class

Miami

Anchorage

Seattle

Mexico City

HoustonBamakoBamako

Casablanca

Madrid

Paris

CopenhagenWarsawWarsaw

Lima

La Paz

RecifeRecife

NEW YORK

757-200112,080-kg (247,100-lb) TOGW*200 two-class passengers

• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from New York.



757-CC-2002 11/6/06 JW/GG




LONDON

New YorkNew York

Luanda

NairobiNairobiLibreville

Muscat

Islamabad

Novosibirsk

Ottawa

Chicago

Dakar

Karachi


• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from London.



757-CC-2001 11/6/06 JW/GG


StartupBoeing

BEIJING

Moscow

Anchorage

DarwinJakarta

Colombo

Karachi

Baku



• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from Beijing.



The 757 is a transcontinental airplane

757-CC-2000 11/6/06 JW/GG




London

Singapore

Beijing

Windhoek

Luanda Jakarta

Hong Kong

Maputo

CasablancaMadrid

Libreville

AccraDUBAI


• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from Dubai.



757-CC-2003 11/6/06 JW/GG



Full passenger payload - Inclusive Tour

Miami

Anchorage

Mexico City

HoustonBamakoBamako

Casablanca

Madrid

Paris

Copenhagen

WarsawWarsaw

Lima La Paz

Recife

NEW YORK

757-200113,890-kg (251,100-lb) TOGW*228 inclusive-tour passengers

• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from New York.


757-300123,830-kg (273,000-lb) MTOW280 inclusive-tour passengers

757-CC-2006 11/7/06 JW/GG




LONDON

New YorkNew York

Luanda

NairobiNairobi

Libreville

Muscat

Islamabad

Novosibirsk

OttawaOttawaChicago

Dakar

Karachi


• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from London.



757-CC-2005 11/7/06 JW/GG




BEIJING

MoscowMoscow

AnchorageAnchorage

Darwin

Jakarta

Colombo

Karachi

Baku


• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from Beijing.



757-CC-2004 11/7/06 JW/GG




LondonLondon

Singapore

Beijing

WindhoekWindhoek

LuandaLuanda JakartaJakarta

Hong Kong

MaputoMaputo

CasablancaCasablanca

MadridMadrid

Libreville

Accra DUBAI


• Typical mission rules.• 85% annual winds.• Airways and traffic allowances included.• Range capability from Dubai.



757-CC-2007 11/7/06 JW/GG

boeing 757-200 - boeing: the boeing · pdf filestartupboeing • two-class seating. •...

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