Boeing Commercial Airplanes
Marketing
P.O. Box 3707
Seattle, WA 98124-2207
www.boeing.com
The statements contained herein are based on good
faith assumptions and provided for general information
purposes only. These statements do not constitute an
offer, promise, warranty or guarantee of performance.
Actual results may vary depending on certain events or
conditions. This document should not be used or relied
upon for any purpose other than that intended by Boeing.
BOEING is a trademark of Boeing Management Company. Printed in U.S.A.
Copyright 2009 Boeing. All rights reserved. FSC LOGO 125992 01/09
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767 FREIGHTER: DIMENSIONS INTERIOR ARRANGEMENTS
Main Deck s 4WENTY
FOUR
X
IN PALLETS OR CONTAINERS
s
M
FT VOLUME CAPACITY
VERSATILE AND CAPABLE
18.6 m 47.6 m #ARGO DOOR
(61 ft 1 in) (156 ft 1 in) M IN X M IN
The 767-300 Freighter does more to help Boeing airplanes continually incorporate new Like all members of the 767 family, the Boeing
air cargo operators succeed. Lighter and technologies and innovations to maximize 767-300F meets all current emissions limits.
s 3EVEN
X
IN PALLETS AND TWO ,$
CONTAINERS
structurally more efficient than other medium performance. Among the benefits to 767-300F Structural, aerodynamic, and propulsion Lower Hold s
M
FT VOLUME CAPACITY
s
M
FT OF BULK EXCLUDED FROM TOTAL VOLUME
widebody freighters, the 767-300F combines the operators are improved aerodynamics and an efficiency together explain its environmental
lowest trip and tonne-kilometer costs in its class advanced main-deck and lower-hold cargo preference over many competing airplane 54.9 m (180 ft 3 in)
"ULK
with superb field performance and reliability. The handling system that is lighter, is more reliable, types. The 767-300F is also very quiet, meeting
result is unrivaled flexibility to serve a spectrum reduces wear, and is fully automated. The ICAO Chapter 4 noise standards. &ORWARD !FT
15.8 m
of regional and intercontinental markets. And 767-300F shares the same pilot type rating (52 ft 0 in)
wherever 767-300F operators fly, the 767 as all 767s as well as a common type rating
familys global success ensures that spares, with all 757s, keeping training costs low and
support equipment, and skilled personnel are allowing airlines to assign flight crews more
readily available. efficiently.
ENVIRONMENTAL PERFORMANCE RANGE CAPABILITY CHARACTERISTICS
Carbon dioxide, g per tonne-km 767-300F
600 Basic Maximum
Maximum taxi weight kg (lb) 185,510 (409,000) 187,330 (413,000)
550 Maximum takeoff weight kg (lb) 185,060 (408,000) 186,880 (412,000)
530
Maximum landing weight kg (lb) 147,870 (326,000) 147,870 (326,000)
500 Maximum zero fuel weight kg (lb) 140,160 (309,000) 140,160 (309,000)
New York Frankfurt Singapore Fuel capacity L (U.S. gal) 90,770 (23,980) 90,770 (23,980)
450 Fuel consumed[1] Liters per tonne-100 km 15.2 15.2
417
Design range[2] nmi 3,125 3,255
Better
400 385 Maximum structural payload[3] kg (lb) 57,260 (126,250) 57,260 (126,250)
Maximum revenue payload[4] kg (lb) 53,660 (118,300) 53,660 (118,300)
350 Cargo volume: Main deck m (ft) 336.5 (11,884)
767-300F DC-10-30F 747-200F 336.5 (11,884)
Lower hold m (ft) 89.3 (3,155) 89.3 (3,155)
s
NMI
KM TRIP s -AXIMUM REVENUE PAYLOAD
Total m (ft) 425.8 (15,039) 425.8 (15,039)
s 4YPICAL MISSION RULES s 4YPICAL MISSION RULES
s -AXIMUM REVENUE PAYLOAD s ANNUAL WINDS [1]
NMI
KM TRIP [3]
3TRUCTURAL PAYLOAD INCLUDES TARE WEIGHT
s !IRWAYS AND TRAFFIC ALLOWANCES INCLUDED [2] [4]
2ANGE AT MAXIMUM REVENUE PAYLOAD 3TRUCTURAL PAYLOAD LESS
KG
LB TARE WEIGHT ALLOWANCE
Home Back Next EXIT
767 FREIGHTER: DIMENSIONS INTERIOR ARRANGEMENTS
Main Deck s 4WENTY
FOUR
X
IN PALLETS OR CONTAINERS
s
M
FT VOLUME CAPACITY
VERSATILE AND CAPABLE
18.6 m 47.6 m #ARGO DOOR
(61 ft 1 in) (156 ft 1 in) M IN X M IN
The 767-300 Freighter does more to help Boeing airplanes continually incorporate new Like all members of the 767 family, the Boeing
air cargo operators succeed. Lighter and technologies and innovations to maximize 767-300F meets all current emissions limits.
s 3EVEN
X
IN PALLETS AND TWO ,$
CONTAINERS
structurally more efficient than other medium performance. Among the benefits to 767-300F Structural, aerodynamic, and propulsion Lower Hold s
M
FT VOLUME CAPACITY
s
M
FT OF BULK EXCLUDED FROM TOTAL VOLUME
widebody freighters, the 767-300F combines the operators are improved aerodynamics and an efficiency together explain its environmental
lowest trip and tonne-kilometer costs in its class advanced main-deck and lower-hold cargo preference over many competing airplane 54.9 m (180 ft 3 in)
"ULK
with superb field performance and reliability. The handling system that is lighter, is more reliable, types. The 767-300F is also very quiet, meeting
result is unrivaled flexibility to serve a spectrum reduces wear, and is fully automated. The ICAO Chapter 4 noise standards. &ORWARD !FT
15.8 m
of regional and intercontinental markets. And 767-300F shares the same pilot type rating (52 ft 0 in)
wherever 767-300F operators fly, the 767 as all 767s as well as a common type rating
familys global success ensures that spares, with all 757s, keeping training costs low and
support equipment, and skilled personnel are allowing airlines to assign flight crews more
readily available. efficiently.
ENVIRONMENTAL PERFORMANCE RANGE CAPABILITY CHARACTERISTICS
Carbon dioxide, g per tonne-km 767-300F
600 Basic Maximum
Maximum taxi weight kg (lb) 185,510 (409,000) 187,330 (413,000)
550 Maximum takeoff weight kg (lb) 185,060 (408,000) 186,880 (412,000)
530
Maximum landing weight kg (lb) 147,870 (326,000) 147,870 (326,000)
500 Maximum zero fuel weight kg (lb) 140,160 (309,000) 140,160 (309,000)
New York Frankfurt Singapore Fuel capacity L (U.S. gal) 90,770 (23,980) 90,770 (23,980)
450 Fuel consumed[1] Liters per tonne-100 km 15.2 15.2
417
Design range[2] nmi 3,125 3,255
Better
400 385 Maximum structural payload[3] kg (lb) 57,260 (126,250) 57,260 (126,250)
Maximum revenue payload[4] kg (lb) 53,660 (118,300) 53,660 (118,300)
350 Cargo volume: Main deck m (ft) 336.5 (11,884)
767-300F DC-10-30F 747-200F 336.5 (11,884)
Lower hold m (ft) 89.3 (3,155) 89.3 (3,155)
s
NMI
KM TRIP s -AXIMUM REVENUE PAYLOAD
Total m (ft) 425.8 (15,039) 425.8 (15,039)
s 4YPICAL MISSION RULES s 4YPICAL MISSION RULES
s -AXIMUM REVENUE PAYLOAD s ANNUAL WINDS [1]
NMI
KM TRIP [3]
3TRUCTURAL PAYLOAD INCLUDES TARE WEIGHT
s !IRWAYS AND TRAFFIC ALLOWANCES INCLUDED [2] [4]
2ANGE AT MAXIMUM REVENUE PAYLOAD 3TRUCTURAL PAYLOAD LESS
KG
LB TARE WEIGHT ALLOWANCE
Home Back Next EXIT
Boeing Commercial Airplanes
Marketing
P.O. Box 3707
Seattle, WA 98124-2207
www.boeing.com
The statements contained herein are based on good
faith assumptions and provided for general information
purposes only. These statements do not constitute an
offer, promise, warranty or guarantee of performance.
Actual results may vary depending on certain events or
conditions. This document should not be used or relied
upon for any purpose other than that intended by Boeing.
BOEING is a trademark of Boeing Management Company. Printed in U.S.A.
Copyright 2009 Boeing. All rights reserved. 125992 01/09
Home Back EXIT
