757-200F
Copyright © 2007 Boeing. All rights reserved.
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Boeing standard-body freighters
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Payload, tons
60
DC-8-63F
40
757-200F
707-320C
727-200F
727-100F
20
0
0
1
2
Range, 1,000 nmi
Copyright © 2007 Boeing. All rights reserved.
3
4
757-200F
Copyright © 2007 Boeing. All rights reserved.
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General arrangement
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757-200F
124 ft 10 in (38.0 m)
49 ft 11 in
(15.2 m)
155 ft 3 in (47.3 m)
Freighter
24 ft 0 in
(7.3 m)
Copyright © 2007 Boeing. All rights reserved.
44 ft 6 in
(13.6 m)
757-200F Ground servicing
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F
E
AC
AS
AS
88- x 125-in (224- x 318-cm)
pallets (15 places)
Copyright © 2007 Boeing. All rights reserved.
757-200F Main Deck pallet &
container positions
Total ULD volume: 6,600 ft3 (187 m3)
Copyright © 2007 Boeing. All rights reserved.
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The 757-200F has two more pallet
positions than the 707
757-200F
707-320C
Copyright © 2007 Boeing. All rights reserved.
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The 757-200F Cargo Doors
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Cargo door (same as 707C and 727F)
134 x 86 in
(340 x 218 cm)
Sill heights
Copyright © 2007 Boeing. All rights reserved.
Maximum, in (cm)
Minimum, in (cm)
158 (401)
150 (381)
Main deck
side door
(top of rollers)
105 (267)
97 (246)
Lower deck
forward door
99 (251)
93 (236)
Lower deck
aft door
757-200F Flight deck features
Oven and hotcup (option)
First observer
STA
297
STA
339
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Flushing toilet
Flight kit
First officer
Rigid barrier
Luggage space
Double supernumerary seat (option)
Sliding door
Captain
Flight kit
Supernumerary seats
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Crew entry door
757-200F Main Deck
Copyright © 2007 Boeing. All rights reserved.
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757-200F Main Deck
Copyright © 2007 Boeing. All rights reserved.
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757-200F Lower hold cargo volume
55 in
(140 cm)
55 in
(140 cm)
42 in (107 cm)
44 in (112 cm)
Forward
Aft
All bulk
700 ft3
(19.8 m3)
Load capacity: 10,300 lb (4,670 kg)
Copyright © 2007 Boeing. All rights reserved.
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Total volume
1,130 ft3
(32.0 m3)
16,300 lb (7,390 kg)
1,830 ft3
(51.8 m3)
757-200F performance summary
Pratt & Whitney engines
Engines
Takeoff thrust*
Main deck cargo
88- x 125-in pallets
Lower hold cargo
Bulk
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight (includes 3,300-lb tare)
Fuel capacity
Volume-limit payload (pallets)**
Design range (MTOW, volume-limit payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW)
Landing field length (MLW)
Approach speed (MLW)
Fuel consumption at volume-limit payload
nmi lb (kg)
1,000 nmi
• Typical mission rules
* Boeing-equivalent thrust
** Volume-limit payload based on 9-lb/ft3 cargo density and 7-lb/ft3 bulk density
Copyright © 2007 Boeing. All rights reserved.
lb/°F
ft3 (m3)
lb (kg)
lb (kg)
lb (kg)
lb (kg)
lb (kg)
U.S. gal (L)
lb (kg)
nmi (km)
ft (m)
ft (m)
ft (m)
kn
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Basic
Maximum
PW2037
36,600/87
PW2040
40,100/87
15
15
1,830 (51.8)
251,000 (113,850)
250,000 (113,400)
210,000 (92,250)
200,000 (90,720)
115,580 (52,430)
11,276 (42,680)
72,210 (32,755)
2,900 (5,370)
0.80
8,950 (2,728)
35,900 (10,940)
5,100 (1,555)
137
1,830 (51.8)
256,000 (116,120)
255,000 (115,660)
210,000 (92,250)
200,000 (90,720)
115,580 (52,430)
11,276 (42,680)
72,210 (32,755)
3,150 (5,830)
0.80
7,700 (2,347)
35,400 (10,790)
5,100 (1,555)
137
10,264 (4,656)
18,308 (8,305)
10,264 (4,656)
18,308 (8,305)
500
lb (kg)
757-200F performance summary
Rolls-Royce Engines
Engines
Takeoff thrust*
Main deck cargo
88- x 125-in pallets
Lower hold cargo
Bulk
Maximum taxi weight
Maximum takeoff weight
Maximum landing weight
Maximum zero fuel weight
Operating empty weight (includes 3,300-lb tare)
Fuel capacity
Volume-limit payload (pallets)**
Design range (MTOW, volume-limit payload)
Cruise Mach
Takeoff field length (SL, 86°F, MTOW)
Initial cruise altitude (MTOW)
Landing field length (MLW)
Approach speed (MLW)
Fuel consumption at volume-limit payload
500 nmi
1,000 nmi
Copyright © 2007 Boeing. All rights reserved.
Basic
Maximum
RB211-535E4
40,200/84
RB211-535E4-B
43,500/77
15
15
ft (m)
ft (m)
ft (m)
kn
1,830 (51.8)
251,000 (113,850)
250,000 (113,400)
210,000 (92,250)
200,000 (90,720)
115,870 (52,560)
11,276 (42,680)
72,210 (32,755)
2,700 (5,000)
0.80
7,100 (2,164)
36,100 (11,000)
4,950 (1,510)
137
1,830 (51.8)
256,000 (116,120)
255,000 (115,660)
210,000 (92,250)
200,000 (90,720)
115,870 (52,560)
11,276 (42,680)
72,210 (32,755)
2,935 (5,435)
0.80
6,900 (2,103)
35,700 (10,880)
4,950 (1,510)
137
lb (kg)
lb (kg)
10,875 (4,933)
19,355 (8,780)
10,875 (4,933)
19,355 (8,780)
lb/°F
ft3 (m3)
lb (kg)
lb (kg)
lb (kg)
lb (kg)
lb (kg)
U.S. gal (L)
lb (kg)
nmi (km)
• Typical mission rules
* Boeing-equivalent thrust
** Volume-limit payload based on 9-lb/ft3 cargo density and 7-lb/ft3 bulk density
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757-200F payload-range capability
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Pratt & Whitney Engines
Payload, 1,000 lb (1,000 kg)
120
255,000-lb (115,660-kg) MTOW
(50)
100
(40)
(30)
250,000-lb (113,400-kg) MTOW
80
Volume limit payload (pallets)
60
40
(10)
20
(0)
0
ty
ci
pa (L) )
ca al 80
el . g 2,6
Fu .S (4
U
76
,2
11
(20)
0
(0)
• Typical mission rules
• 200-nmi alternate
• 6.7 lb per U.S. gal fuel density
Copyright © 2007 Boeing. All rights reserved.
1
(2)
2
3
(4)
4
(6)
Range, 1,000 nmi (1,000 km)
5
(8)
6
(10)
757-200F payload-range capability
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Rolls-Royce engines
Payload, 1,000 lb (1,000 kg)
120
(50)
255,000-lb (115,660-kg) MTOW
100
250,000-lb (113,400-kg) MTOW
(40)
80
(30)
40
(10)
20
(0)
0
ty
ci
pa L) )
ca l ( 60
el . ga 2,6
Fu .S 6 (4
U 7
,2
11
(20)
Volume limit payload (pallets)
60
0
(0)
• Typical mission rules
• 200-nmi alternate
• 6.7 lb per U.S. gal fuel density
Copyright © 2007 Boeing. All rights reserved.
1
(2)
2
3
(4)
4
(6)
Range, 1,000 nmi (1,000 km)
5
(8)
6
(10)
Mission profile
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Typical mission rules
5% mission
fuel allowance
Climb
LRC
100 nmi
f
0
,5
1
to
d
n
c
s
e
D
h
c
ro
p
a
d
e
is
M
P
A
f)
0
,5
1
a
d
e
p
s
b
lim
c
to
(V
i)
m
l(5
d
n
h
c
a
ro
p
A
f)
,5
t1
in
m
0
(3
ld
h
c
a
ro
p
A
v
s
e
)fro
m
(5
in
x
a
T
Still air range
Block time and fuel
• Standard day
• Fuel density, 6.7 lb per U.S. gal
• Nominal performance
Copyright © 2007 Boeing. All rights reserved.
Approach hold (30 min at 1,500 ft)
i)
m
l(5
d
n
h
c
a
ro
p
A
n
k
2
e
c
f;a
0
,5
1
to
b
lim
C
b
lim
C
Approach and land (5 min)
f
0
,5
1
to
d
n
c
s
e
D
c
n
w
o
la
e
fu
Descend to 1,500 ft
d
p
s
b
im
to
lra
e
c
A
n
k
5
2
,fa
0
1
to
b
lim
C
n
o
is
m
%
5
Missed approach
(V to climb speed at 1,500 ft)
n
k
0
5
2
to
lra
c
e
D
Taxi in (5 min) from reserves
,f
0
1
to
d
n
c
s
e
D
Approach and land (5 min)
b
lim
C
Decelerate to 250 kn
Descend to 1,500 ft
Long-range cruise
(LRC)
Reserves
Descend to 10,000 ft
Climb
Climb to 10,000 ft at 250 kn
Accelerate to climb speed
Climb to 1,500 ft; accel to 250 kn
Takeoff (to 35 ft)
Taxi out (9 min)
Mission
200 nmi
Typical reserves
Range capability from Los Angeles
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Volume limit payload
757-200 Freighter
255,000-lb (115,660-kg) MTOW
Anchorage
Juneau
757-200 Freighter
Seattle Chicago
250,000-lb (113,400-kg) MTOW
Montreal
New York
Bermuda
Miami
Honolulu
LOS ANGELES
Mexico City
Panama City
•
•
•
•
•
•
PW2037/2040 engines
Typical mission rules
Airways and traffic allowances included
Nominal performance
85% annual winds
3,300-lb (1,500-kg) tare weight
Copyright © 2007 Boeing. All rights reserved.
Range capability from New York
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Volume limit payload
757-200 Freighter
Reykjavik
255,000-lb (115,660-kg) MTOW
Juneau
London
Madrid
757-200 Freighter
Seattle
250,000-lb (113,400-kg) MTOW
Terceira
Los Angeles
NEW YORK
Miami
Mexico City
Panama City
•
•
•
•
•
•
PW2037/2040 engines
Typical mission rules
Airways and traffic allowances included
Nominal performance
85% annual winds
3,300-lb (1,500-kg) tare weight
Copyright © 2007 Boeing. All rights reserved.
Quito
Belem
Range capability from Miami
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Volume limit payload
757-200 Freighter
255,000-lb (115,660-kg) MTOW
Seattle
757-200 Freighter
250,000-lb (113,400-kg) MTOW
Chicago
Los Angeles
Mexico City
Montreal
New York
Terceira
MIAMI
Panama City
Caracas
Bogota
Quito
Manaus
•
•
•
•
•
•
PW2037/2040 engines
Typical mission rules
Airways and traffic allowances included
Nominal performance
85% annual winds
3,300-lb (1,500-kg) tare weight
Copyright © 2007 Boeing. All rights reserved.
Lima
Belem
Range capability from London
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Volume limit payload
757-200 Freighter
255,000-lb (115,660-kg) MTOW
757-200 Freighter
250,000-lb (113,400-kg) MTOW
Reykjavik
Gander
Moscow
Stockholm
Ashgabat
LONDON
Terceira
Madrid
Baku
Athens
Bahrain
Dubai
Cairo
Jeddah
Khartoum
Dakar
•
•
•
•
•
•
PW2037/2040 engines
Typical mission rules
Airways and traffic allowances included
Nominal performance
85% annual winds
3,300-lb (1,500-kg) tare weight
Copyright © 2007 Boeing. All rights reserved.
Ndjamena
Abidjan
Lagos
Range capability from Singapore
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Volume limit payload
Beijing
757-200 Freighter
255,000-lb (115,660-kg) MTOW
Karachi
757-200 Freighter
Tokyo
Kabul
Delhi
Mumbai
Calcutta
Hong Kong
Manila
250,000-lb (113,400-kg) MTOW
Guam
Colombo
SINGAPORE
Port Moresby
Darwin
Perth
•
•
•
•
•
•
PW2037/2040 engines
Typical mission rules
Airways and traffic allowances included
Nominal performance
85% annual winds
3,300-lb (1,500-kg) tare weight
Copyright © 2007 Boeing. All rights reserved.
Range capability from Tokyo
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Volume limit payload
Anchorage
757-200 Freighter
255,000-lb (115,660-kg) MTOW
757-200 Freighter
Ulaanbaatar
250,000-lb (113,400-kg) MTOW
Vladivostok
Beijing
Chengdu
Kunming
Seoul
TOKYO
Hong Kong
Bangkok
Manila
Guam
Davao
•
•
•
•
•
•
PW2037/2040 engines
Typical mission rules
Airways and traffic allowances included
Nominal performance
85% annual winds
3,300-lb (1,500-kg) tare weight
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Port Moresby
757 Flight Deck
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1/22/2008