The 767-300BCF is a great fit for
the medium-widebody freighter market
The ideal 707, DC-8 and DC-10 replacement
COPYRIGHT © 2006 THE BOEING COMPANY
767-300BCF conversion overview
Typical options
Class E main deck
and lower lobe
One minute smoke
detection system
Remove passenger
interior and lining
Install cargo linings
Thicker cargo liners
Outside operable
number 2 window (RH)
Revised control cable routing
Main deck temperature control
9-G rigid cargo barrier
and 24th pallet position
Fuselage and wing
structural changes
Replace floor structure with
stronger freighter floor system
Cargo door and surround
structure same as -300F
with external control panel
Gear amendments for
increased weights for
some aircraft
Installation of supernumerary
BFE seats
Provisions for powered
BFE CHS
Remove SATCOM
COPYRIGHT © 2010 THE BOEING COMPANY
Window
plugs
Modified ECS and
A/C for live animal
carriage
FWD lower lobe air conditioning
and bulk cargo ventilation fan
Deactivate passenger doors and
emergency exits except door 1L
Rev 2 | 2
767 Freighter cargo door arrangement
70 in
(178 cm)
69 in
(175 cm)
70 in
(178 cm)
69 in
(175 cm)
Large or standard
forward lower cargo
compartment door
(STA 548)
Rev 2 | 6
COPYRIGHT © 2010 THE BOEING COMPANY
767-300BCF cargo arrangements
Main deck configuration same as 767-300F
Side-by-side 88- x 125-in
Main deck ULD loading configuration
Main Deck
Lower Hold
Total
3,840 cu. ft.
(108.7 cu. m.)
ULD type
Volume
Contoured Type-A ULD 11,044 cu. ft.
@ 502 cu. ft. each
2
Standard A2 ULD
@ 420 cu. ft. each
Total =
134- x 103-in door
(4) 96- x 125-in @ 415 = 1,660 cu. ft.
134- x 69-in door
Qty
22
840 cu. ft.
11,884 cu. ft. (336.5 cu. m.)
(14) LD-2 @ 125 = 1,750 cu. ft.
70- x 69-in door
Bulk
Bulk 430 cu. ft.
Rev 2 | 8
COPYRIGHT © 2010 THE BOEING COMPANY
767-300BCF longitudinal loading with
M1-size containers
11 M1-size containers
(maximum envelope)
2 standard A2 ULD
(maximum envelope)
96 in
(244 cm)
81.75 in
(208 cm)
96 in
(244 cm)
125 in
(318 cm)
125 in
(318 cm)
1C
1
2
3
4
5
6
7
8
9
10
88 in
(224 cm)
11
2C
Side
cargo
door
• Optional engine carriage
in 5th and 6th positions
Rev 2 | 10
COPYRIGHT © 2010 THE BOEING COMPANY
767-300BCF transverse loading with
M-size pallets
14 M-size pallets
(maximum envelope)
2 standard A2 ULD
(maximum envelope)
96 in
(244 cm)
81.75 in
(208 cm)
125 in
(318 cm)
96 in
(244 cm)
125 in
(318 cm)
1C
1
2
3
4
5
6
7
8
9
10
11
12
13
88 or 96 in
(224 or 244 cm)
14
2C
Side
cargo
door
• 14 A-size containers/pallets
also available in transverseloading configuration
Rev 2 | 12
COPYRIGHT © 2010 THE BOEING COMPANY
The 767-300BCF main deck accommodates
universal containers and pallets
96 in
(243.8 cm)
96 in
(243.8 cm)
238.5 in
(605.8 cm)
G-code pallet*
*Loads contoured as required for clearance
• All units in inches (centimeters)
• Includes Military pallet capability (88x108-in)
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 9
767-300BCF cargo arrangement with
88x108-in pallets/containers
Main Deck
134- x 103-in door
Side-by-side 88- x 108-in
Main deck ULD loading configuration
Qty
24
ULD type
Volume
Contoured Type-B ULD 10,416 cu. ft.
@ 434 cu. ft. each
2
Standard Type-B ULD
@ 363 cu. ft. each
Total =
726 cu. ft.
11,142 cu. ft. (315.5 cu. m.)
Rev 2 | 13
COPYRIGHT © 2010 THE BOEING COMPANY
Flight compartment arrangement with rigid
cargo barrier same as delivered on 767-300F
Supernumerary seats (BFE) installation option
Lavatory
Stowage (typical)
Rigid Cargo
Barrier (RCB)
Access door to cargo bay
Galley (BFE) or optional
“close-out panel”
Rigid barrier
Stowage (typical)
Entry door
Step (up into flight
compartment)
Main deck cargo
door control panel
Rev 2 | 3
COPYRIGHT © 2010 THE BOEING COMPANY
Supernumerary configuration
same as 767-300F
Rev 2 | 4
COPYRIGHT © 2010 THE BOEING COMPANY
Typical 767-300F/BCF galley (BFE)
Main deck cargo
door control panel
Working surface with sump
Cargo bay access door
Waste container and
gray water tank
Insert envelope
(potential cold-food storage
and miscellaneous stowage)
Optional close-out panel in
lieu of BFE galley
Up
INBD
Rev 2 | 5
COPYRIGHT © 2010 THE BOEING COMPANY
767-300BCF main deck cargo
compartment
Rev 2 | 7
COPYRIGHT © 2010 THE BOEING COMPANY
The four primary containers
Lower hold of the 767
(2) LD-2 containers
Pallet
LD-4 container
LD-3 container
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 14
767-300BCF and 747 interline capability
96-in x 125-in pallets and containers
96 in
(244 cm)
Rev 2 | 11
COPYRIGHT © 2010 THE BOEING COMPANY
767-300BCF performance summary
Product Development Study
General Electric Engines
Maximum Taxi Weight
Maximum Takeoff Weight
Maximum Landing Weight
Maximum Zero Fuel Weight
Estimated OEW (including tare)
Tare
Fuel Capacity
Revenue Payload
Design Range
1
Total Volume
Density
Main Deck Volume (Pallets)
88x125 x86
88x125 x odd
Lower Deck Volume
96x125
LD-2
Bulk
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
767-300ER BCF
CF6-80C2B6F
Power CHS
(Maximum Weights)
(413,000)
187,330
(412,000)
186,880
(326,000)
147,870
(309,000)
140,160
(194,300)
88,130
(10,680)
4,840
(23,980)
90,770
Cargo Door Size - Fwd Lower Hold
Cargo Door Size - Aft Lower Hold
• Typical mission rules
• Nominal fuel burn + 4%
COPYRIGHT © 2010 THE BOEING COMPANY
767-300 BCF
CF6-80A2
Manual CHS
(Non-ER)
(352,200)
159,750
(351,000)
159,210
(300,000)
136,070
(278,000)
126,090
(198,150)
89,870
(18,480)
8,380
(16,700)
63,210
kg (lb)
nmi (km)
52,020
3,100
(114,700)
(5,741)
43,400
3,600
(95,700)
(6,667)
36,210
2,200
(79,850)
(4,074)
3
m (ft3)
3
kg/m (lb/ft3)
445.3
116.8
(15,724)
(7.3)
454.9
95.4
(16,064)
(6.0)
454.9
79.6
(16,064)
(5.0)
(11,884)
336.5
(11,884)
336.5
3
m (ft3)
Quantity
336.5
Quantity
2
767-300ER BCF
CF6-80C2B
Manual CHS
(Baseline Weights)
(409,000)
185,510
(408,000)
185,060
(320,000)
145,140
(295,000)
133,800
(199,300)
90,400
(18,480)
8,380
(23,980)
90,770
3
3
m (ft )
Quantity
Quantity
96.6
3
m (ft3)
12.2
(11,884)
22
22
22
2
2
2
(3,410)
(3,750)
106.2
4
14
(430)
Large
Standard
12.2
(3,750)
106.2
0
30
0
30
(430)
Large
Standard
12.2
(430)
Standard
Standard
Rev 2 | 15
767-300BCF performance summary
Product Development Study
Pratt and Whitney Engines
Maximum Taxi Weight
Maximum Takeoff Weight
Maximum Landing Weight
Maximum Zero Fuel Weight
Estimated OEW (including tare)
Tare
Fuel Capacity
Revenue Payload
Design Range
1
Total Volume
Density
Main Deck Volume (Pallets)
88x125 x86
88x125 x odd
Lower Deck Volume
96x125
LD-2
Bulk
2
Cargo Door Size - Fwd Lower Hold
Cargo Door Size - Aft Lower Hold
• Typical mission rules
• Nominal fuel burn + 4%
COPYRIGHT © 2010 THE BOEING COMPANY
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
L (U.S. gal)
767-300ER BCF
PW4062
Power CHS
(Maximum Weights)
(413,000)
187,330
(412,000)
186,880
(326,000)
147,870
(309,000)
140,160
(194,900)
88,400
(10,680)
4,840
(23,980)
90,774
767-300ER BCF
PW4060
Manual CHS
(Baseline Weights)
(409,000)
185,510
(408,000)
185,060
(320,000)
145,140
(295,000)
133,800
(199,900)
90,670
(18,480)
8,380
(23,980)
90,774
767-300BCF
JT9D-7R4E
Manual CHS
(Non-ER)
(352,200)
159,750
(351,000)
159,210
(300,000)
136,070
(278,000)
126,090
(198,750)
90,150
(18,480)
8,380
(16,700)
63,216
kg (lb)
nmi (km)
51,750
3,113
(114,100)
(5,765)
43,130
3,570
(95,100)
(6,612)
35,940
2,202
(79,250)
(4,078)
3
m (ft3)
3
kg/m (lb/ft3)
445.3
116.2
(15,724)
(7.3)
454.9
94.8
(16,064)
(5.9)
454.9
79.0
(16,064)
(4.9)
(11,884)
336.5
(11,884)
336.5
3
m (ft3)
Quantity
Quantity
3
336.5
22
2
m (ft3)
Quantity
Quantity
96.6
3
m (ft3)
12.2
22
2
(3,410)
(3,750)
106.2
4
14
Large
Standard
12.2
(3,750)
106.2
0
30
(430)
(11,884)
22
2
0
30
(430)
Large
Standard
12.2
(430)
Standard
Standard
Rev 2 | 16
767-300BCF payload-range capability
General Electric Engines
Revenue Payload, 1,000 kg (1,000 lb)
(140)
60
(120)
Maximum Weights
50
186,880-kg(412,000-lb)MTOW
140,160-kg(309,000-lb)MZFW
(100)
40
Baseline Weights
(80)
185,066-kg(408,000-lb)MTOW
133,810-kg(295,000-lb)MZFW
30
(60)
Non-ER*
159,211-kg(351,000-lb)MTOW
126,099-kg(278,000-lb)MZFW
20
(40)
(20)
0
10
0
0
0
1
(1)
(2)
2
(3)
3
(4)
(5)
4
(6)
(7)
5
(8)
(9)
6
(10)
(11)
7
(12)
(13)
8
(14)
(15)
Range, 1,000 nmi(km)
• Typical mission rules
• 200 nmi alternate
* Product Development Study
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 17
Range capability from Los Angeles
Revenue Payload
767-300ER BCF
186,880-kg (412,000-lb) MTOW
140,160-kg (309,000-lb) MZFW
52,072-kg (114,700-lb) Payload
Anchorage
767-300ER BCF
185,060-kg (408,000-lb) MTOW
133,8000-kg (295,000-lb) MZFW
43,409-kg (95,700-lb) Payload
767-300 BCF*
159,210-kg (351,000-lb) MTOW
126,090-kg (278,000-lb) MZFW
36,219-kg (79,850-lb) Payload
New York
Seattle
LOS ANGELES
Miami
Honolulu
Mexico City Caracas
Panama City
Quito
•
•
•
•
Lima
GE engines
Typical mission rules
85% annual winds
Nominal fuel burn + 4%
* Product Development Study
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 18
Range capability from Anchorage
Revenue Payload
Helsinki
767-300ER BCF
Reykjavik
186,880-kg (412,000-lb) MTOW
140,160-kg (309,000-lb) MZFW
52,072-kg (114,700-lb) Payload
767-300ER BCF
185,060-kg (408,000-lb) MTOW
133,8000-kg (295,000-lb) MZFW
43,409-kg (95,700-lb) Payload
Beijing
Montreal
Shanghai
New York
767-300 BCF*
159,210-kg (351,000-lb) MTOW
126,090-kg (278,000-lb) MZFW
36,219-kg (79,850-lb) Payload
Tokyo
ANCHORAGE
Miami
Los Angeles
Mexico City
Honolulu
•
•
•
•
GE engines
Typical mission rules
85% annual winds
Nominal fuel burn + 4%
* Product Development Study
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 19
Range capability from Tokyo
Revenue Payload
767-300ER BCF
186,880-kg (412,000-lb) MTOW
140,160-kg (309,000-lb) MZFW
52,072-kg (114,700-lb) Payload
Anchorage
767-300ER BCF
185,060-kg (408,000-lb) MTOW
133,8000-kg (295,000-lb) MZFW
43,409-kg (95,700-lb) Payload
Beijing
767-300 BCF*
159,210-kg (351,000-lb) MTOW
126,090-kg (278,000-lb) MZFW
36,219-kg (79,850-lb) Payload
Chengdu
TOKYO
Hong Kong
Singapore
GE engines
Typical mission rules
85% annual winds
Nominal fuel burn + 4%
Guam
Davao
Darwin
Port Moresby
* Product Development Study
COPYRIGHT © 2010 THE BOEING COMPANY
Honolulu
Shanghai
Yangon
Manila
•
•
•
•
Sapporo
Rev 2 | 20
Range capability from Dubai
Revenue Payload
767-300ER BCF
186,880-kg (412,000-lb) MTOW
140,160-kg (309,000-lb) MZFW
52,072-kg (114,700-lb) Payload
767-300ER BCF
London
Moscow
Beijing
Madrid
185,060-kg (408,000-lb) MTOW
133,8000-kg (295,000-lb) MZFW
43,409-kg (95,700-lb) Payload
Baku
Cairo
767-300 BCF*
159,210-kg (351,000-lb) MTOW
126,090-kg (278,000-lb) MZFW
36,219-kg (79,850-lb) Payload
DUBAI
Chengdu
Delhi
Hong Kong
Jeddah
Yangon
Mumbai
Khartoum
Male
Singapore
Brazzaville
•
•
•
•
GE engines
Typical mission rules
85% annual winds
Nominal fuel burn + 4%
Harare
Antananarivo
* Product Development Study
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 21
Range capability from London
Revenue Payload
767-300ER BCF
186,880-kg (412,000-lb) MTOW
140,160-kg (309,000-lb) MZFW
52,072-kg (114,700-lb) Payload
767-300ER BCF
185,060-kg (408,000-lb) MTOW
133,8000-kg (295,000-lb) MZFW
43,409-kg (95,700-lb) Payload
Montreal
New York
Reykjavik
Delhi
Moscow
767-300 BCF*
LONDON
159,210-kg (351,000-lb) MTOW
126,090-kg (278,000-lb) MZFW
36,219-kg (79,850-lb) Payload
Dubai
Jeddah
Khartoum
Dakar
•
•
•
•
GE engines
Typical mission rules
85% annual winds
Nominal fuel burn + 4%
Abidjan
* Product Development Study
COPYRIGHT © 2010 THE BOEING COMPANY
Rev 2 | 22
767-200ER/-300ER Flight Deck
StartupBoeing
Copyright © 2007 Boeing. All rights reserved.
1/22/2008