747-400 Boeing Converted Freighter

747-400 Boeing Converted Freighter
High-value, low economic risk replacement for earlier tri and quadengine freighters
COPYRIGHT © 2006 THE BOEING COMPANY
747-400BCF conversion overview
Retain existing crew rest
8 upper deck supernumeraries
Deletion of the aft,
straight stairway and
installation of the ladder
Revised Integrated Display
System software
MTW
MTOW
MLW
MZFW
873,000 lb (395,986 kg)
870,000 lb (394,625 kg)
652,000 lb (295,742 kg)
610,000 lb (276,691 kg)
Replacement of the aft,
upper deck floor beams
with tension ties
Strengthening of the wing gear
side struts and wing-to-body joint
Vacuum waste system
Window plugs
Full main deck lining
for Class E cargo
(similar to 747-400F)
Remove
flight deck door
Class C lower lobe
Add 747-400F
cargo door and
surround structure
Fwd and aft lower
lobe air-conditioning
Deactivate all main deck
entry doors except 1L and 5L
Main deck and lower
lobe animal carriage
Provisions for selected
cargo-handling system
290 lb/in running
load over wing
Install 400F-type Main
Deck Cargo floor beams
Rerouting of mechanical
flight controls
Rev 2| 1
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF cargo arrangements
86-in high cargo
118-in high cargo
Main Deck
Sta
(1) 96- x 125-in Pallet at 532 cu. ft.
1850
(8) 96- x 125-in Pallets at 549 cu. ft.
(21) M1H Pallets at 750 cu. ft. (118-in high)
Main Deck Total
20,674 cu. ft. (585.4 cu. m.)
Forward
Aft
Bulk
688 cu. ft.
Lower Hold
(9) 96- x 125-in Pallets at 415 cu. ft.
Bulk Cargo 688 cu. ft.
Lower Hold Total
4,423 cu. ft. (125.2 cu. m.)
Note: AS 1825 volumes used
Total Cargo Volume = 25,097 (710.7 cu. m.)
Rev 2| 7
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF basic upper deck layout
Emergency Door
Sta
690
780
Lit. Pockets (2) Places
Provisions Only
Cabin Control Panel
MDA
4U Lavatory
Access Door
Curtain
Crew Rest
(2 Bunks)
Down
180o
Maximum
Open Angle
MDA
MDA
747-400F Type Galley
Track Mounted
747-400F Type
Stowable Ladder and Cutout
Lit. Pockets (2) Places
Provisions Only
Emergency Equipment
Provisions for main deck access
oxygen bottles & masks
Sidewall Stowage Unit (Typ)
Buyer Furnished Equipment
(customer responsible for
certification)
Two 10-Person
Life Rafts
8 Supernumerary Seats
Rev 2| 2
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF maximum optional upper
deck layout
Emergency Door
Sta
690
780
Lit. Pockets (2) Places
Provisions Only
Cabin Control Panel
MDA
4U Lavatory
Access Door
Curtain
Crew Rest
(2 Bunks)
Down
180o
Maximum
Open Angle
MDA
MDA
747-400F Type Galley
Track Mounted
747-400F Type
Stowable Ladder and Cutout
Lit. Pockets (2) Places
Provisions Only
Emergency Equipment
Provisions for main deck access
oxygen bottles & masks
Sidewall Stowage Unit (Typ)
Buyer Furnished Equipment
(customer responsible for
certification)
Three 10-Person
Life Rafts
19 Supernumerary Seats
Rev 2| 4
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF upper deck modification
Restraint strap
Crown net
STA
880
STA
902
Remove floor beams
install tension ties, and
reroute control cables
10 ft
*
~20,674 ft3 main deck cargo volume
(all pallet configuration)
Rev 2| 5
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF – Typical upper deck
configuration
Rev 2| 3
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF Main Deck
Rev 2| 6
COPYRIGHT © 2010 THE BOEING COMPANY
747-400BCF performance summary
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
Total Volume
Density
Main Deck Volume (Pallets)
96x125 x96 (BCF/SF 96x125 x86)
96x125 x118
Lower Deck Volume
96x125
LD-1
Bulk
• Typical mission rules
• Nominal fuel burn + 4%
COPYRIGHT © 2010 THE BOEING COMPANY
747-200SF
747-400BCF
CF6-50E1
CF6-80C2B1F
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
379,203
377,842
285,763
267,619
160,939
5,130
(836,000)
(833,000)
(630,000)
(590,000)
(354,810)
(11,310)
395,986
394,625
295,742
276,691
168,850
5,266
(873,000)
(870,000)
(652,000)
(610,000)
(372,250)
(11,610)
L (U.S. gal)
196,974
(52,035)
203,523
(53,765)
kg (lb)
nmi (km)
106,680
3,174
(235,190)
(5,878)
107,842
4,091
(237,750)
(7,577)
m3 (ft3)
kg/m3 (lb/ft3)
m3 (ft3)
Quantity
704.4
151.4
570.4
(24,877)
(9.5)
(20,142)
710.7
151.9
585.4
(25,097)
(9.5)
(20,674)
Quantity
3
3
m (ft )
Quantity
Quantity
m3 (ft3)
8
9
21
21
105.8
(3,735)
105.8
9
0
28.3
(3,735)
9
0
(1,000)
19.5
(688)
Rev 2| 9
747-400BCF performance summary
Pratt and Whitney Engines
747-200SF
747-400BCF
JT9D-7R4G2
PW4062
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
kg (lb)
379,203
377,842
285,763
267,619
159,397
5,130
(836,000)
(833,000)
(630,000)
(590,000)
(351,410)
(11,310)
395,986
394,625
295,742
276,691
168,895
5,266
(873,000)
(870,000)
(652,000)
(610,000)
(372,350)
(11,610)
L (U.S. gal)
198,393
(52,410)
204,355
(53,985)
kg (lb)
nmi (km)
108,223
3,435
(238,590)
(6,362)
107,796
4,100
(237,650)
(7,593)
m3 (ft3)
kg/m3 (lb/ft3)
704.4
153.6
(24,877)
(9.6)
710.7
151.8
(25,097)
(9.5)
570.4
(20,142)
585.4
(20,674)
96x125 x96 (BCF/SF 96x125 x86)
m3 (ft3)
Quantity
96x125 x118
Quantity
Maximum Taxi Weight
Maximum Takeoff Weight
Maximum Landing Weight
Maximum Zero Fuel Weight
Estimated OEW (including tare)
Tare
Fuel Capacity
Revenue Payload
Design Range
Total Volume
Density
Main Deck Volume (Pallets)
Lower Deck Volume
96x125
LD-1
Bulk
• Typical mission rules
• Nominal fuel burn + 4%
COPYRIGHT © 2010 THE BOEING COMPANY
3
3
m (ft )
Quantity
Quantity
m3 (ft3)
8
9
21
21
105.8
(3,735)
105.8
9
0
28.3
(3,735)
9
0
(1,000)
19.5
(688)
Rev 2| 10
747-400BCF performance summary
Rolls Royce Engines
747-200SF
747-400BCF
RB211-524D4
RB211-524G
Maximum Taxi Weight
kg (lb)
379,203
(836,000)
395,986
(873,000)
Maximum Takeoff Weight
kg (lb)
377,842
(833,000)
394,625
(870,000)
Maximum Landing Weight
kg (lb)
285,763
(630,000)
295,742
(652,000)
Maximum Zero Fuel Weight
kg (lb)
267,619
(590,000)
276,691
(610,000)
Estimated OEW (including tare)
kg (lb)
163,389
(360,210)
169,507
(373,700)
kg (lb)
5,130
(11,310)
5,266
(11,610)
L (U.S. gal)
198,393
(52,410)
204,355
(53,985)
kg (lb)
104,231
(229,790)
107,184
(236,300)
nmi (km)
3,421
(6,336)
4,052
(7,504)
m3 (ft3)
kg/m3 (lb/ft3)
m3 (ft3)
Quantity
Quantity
m3 (ft3)
Quantity
Quantity
704.4
148.0
570.4
(24,877)
(9.2)
(20,142)
710.7
150.9
585.4
(25,097)
(9.4)
(20,674)
m3 (ft3)
28.3
Tare
Fuel Capacity
Revenue Payload
Design Range
Total Volume
Density
Main Deck Volume (Pallets)
96x125 x96 (BCF/SF 96x125 x86)
96x125 x118
Lower Deck Volume
96x125
LD-1
Bulk
• Typical mission rules
• Nominal fuel burn + 4%
COPYRIGHT © 2010 THE BOEING COMPANY
8
21
105.8
9
21
(3,735)
105.8
9
0
(3,735)
9
0
(1,000)
19.5
(688)
Rev 2| 11
Typical 747-400BCF
payload-range capability
Revenue Payload, 1,000 kg (1,000 lb)
(320)
140
(280)
120
(240)
747-400BCF
394,625 -kg (870,000-lb) MTOW
276,691 -kg (610,000-lb) MZFW
100
(200)
747-200SF
80
377,842 -kg (833,000-lb) MTOW
267,619 -kg (590,000-lb) MZFW
(160)
60
(120)
(80)
40
(40)
20
0
0
0
0
1
(1)
• Typical mission rules
• 200 nmi alternate
(2)
2
(3)
3
(4)
(5)
4
(6)
(7)
5
(8)
(9)
6
(10)
(11)
7
(12)
(13)
8
(14)
(15)
9
(16)
(17)
Range, 1,000 nmi (1,000 km)
Rev 2| 8
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Moscow
Revenue Payload
747-400BCF
Anchorage
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
New York
Tokyo
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Beijing
Seoul
Shanghai
London
MOSCOW
Hong Kong
Delhi
Mumbai
Singapore
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Rev 2| 12
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Anchorage
Revenue Payload
Frankfurt
Frankfurt
747-400BCF
Moscow
Moscow
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
London
London
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Beijing
Beijing
Shanghai
Shanghai
Tokyo
Tokyo
ANCHORAGE
Caracas
Caracas
Miami
Miami
Honolulu
Honolulu
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Rev 2| 13
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Hong Kong
Revenue Payload
Anchorage
Anchorage
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Moscow
Moscow
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Dubai
Dubai
Mumbai
Mumbai
Seoul
Seoul
HONG KONG
Kuala
Lumpur
Kuala Lumpur
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Sydney
Sydney
Rev 2| 14
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Kuala Lumpur
Revenue Payload
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Seoul
Seoul
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Dubai
Dubai
Mumbai
Mumbai
KUALA LUMPUR
Tanandava
Tanandava
Sydney
Sydney
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Rev 2| 15
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from London
Revenue Payload
747-400BCF
Vancouver
Vancouver
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Anchorage
Anchorage
Beijing
Beijing
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Miami
Miami
New
New York
York
Delhi
Delhi
LONDON
Mumbai
Mumbai
Caracas
Caracas
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Lusaka
Lusaka
Rev 2| 16
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Luxembourg
Revenue Payload
Anchorage
Anchorage
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Beijing
Beijing
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
New
New York
York
Delhi
Delhi
London
London
Mumbai
Mumbai
LUXEMBOURG
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Lusaka
Lusaka
Rev 2| 17
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from New York
Revenue Payload
747-400BCF
Moscow
Moscow
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Anchorage
Anchorage
London
London
Vancouver
Vancouver
NEW YORK
Miami
Miami
Caracas
Caracas
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Lima
Lima
Rio
Janeiro
Rio De
De Janeiro
Rev 2| 18
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Seoul
Revenue Payload
747-400BCF
Stockholm
Stockholm
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Vancouver
Vancouver
Moscow
Moscow
Anchorage
Anchorage
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Dubai
Dubai
Honolulu
Honolulu
SEOUL
Mumbai
Mumbai
Singapore
Singapore
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Sydney
Sydney
Rev 2| 19
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Shanghai
Revenue Payload
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Helsinki
Helsinki
Anchorage
Anchorage
Moscow
Moscow
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Dubai
Dubai
SHANGHAI
Tokyo
Tokyo
Mumbai
Mumbai
Singapore
Singapore
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Sydney
Sydney
Rev 2| 20
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Singapore
Revenue Payload
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Seoul
Seoul
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Dubai
Dubai
Mumbai
Mumbai
SINGAPORE
Tanandava
Tanandava
Sydney
Sydney
Auckland
Auckland
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Rev 2| 21
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Tel Aviv
Revenue Payload
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Beijing
Beijing
747-200SF
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
London
London
Moscow
Moscow
Shanghai
Shanghai
Hong
Hong Kong
Kong
TEL AVIV
Delhi
Delhi
Mumbai
Mumbai
Singapore
Singapore
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Johannesburg
Johannesburg
Rev 2| 22
COPYRIGHT © 2010 THE BOEING COMPANY
Range capability from Tokyo
Revenue Payload
747-400BCF
394,625-kg (870,000-lb) MTOW
107,842-kg (237,750-lb) Payload
Moscow
Moscow
Vancouver
Vancouver
Anchorage
Anchorage
747-200SF
Los
Los Angeles
Angeles
377,842-kg (833,000-lb) MTOW
106,680-kg (235,190-lb) Payload
Mumbai
Mumbai
TOKYO
Hong
Hong Kong
Kong
Kuala
Kuala Lumpur
Lumpur
• Typical mission rules
• 85% annual winds
• Nominal fuel burn + 4%
Sydney
Sydney
Rev 2| 23
COPYRIGHT © 2010 THE BOEING COMPANY
747 Flight Deck
StartupBoeing
Copyright © 2007 Boeing. All rights reserved.
1/22/2008