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1 F
2 Boeing standard-body freighters Payload, tons 60 DC-8-63F F C F F Range, 1,000 nmi
3 F
4 General arrangement F 124 ft 10 in (38.0 m) 49 ft 11 in (15.2 m) 155 ft 3 in (47.3 m) Freighter 44 ft 6 in (13.6 m) 24 ft 0 in (7.3 m)
5 F Ground servicing F E AC AS AS 88- x 125-in (224- x 318-cm) pallets (15 places)
6 F Main Deck pallet & container positions Total ULD volume: 6,600 ft 3 (187 m 3 )
7 The F has two more pallet positions than the F C
8 The F Cargo Doors Cargo door (same as 707C and 727F) 134 x 86 in (340 x 218 cm) Sill heights 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
9 F Flight deck features Oven and hotcup (option) First observer STA 297 STA 339 Flushing toilet Flight kit First officer Rigid barrier Luggage space Double supernumerary seat (option) Sliding door Captain Flight kit Supernumerary seats Crew entry door
10 F Main Deck
11 F Main Deck
12 F Lower hold cargo volume 55 in (140 cm) 55 in (140 cm) 42 in (107 cm) 44 in (112 cm) Forward Aft All bulk Total volume 700 ft 3 (19.8 m 3 ) 1,130 ft 3 (32.0 m 3 ) 1,830 ft 3 (51.8 m 3 ) Load capacity: 10,300 lb (4,670 kg) 16,300 lb (7,390 kg)
13 F performance summary Pratt & Whitney engines Engines Takeoff thrust* lb/ F Main deck cargo 88- x 125-in pallets Lower hold cargo Bulk ft 3 (m 3 ) Maximum taxi weight lb (kg) Maximum takeoff weight lb (kg) Maximum landing weight lb (kg) Maximum zero fuel weight lb (kg) Operating empty weight (includes 3,300-lb tare) lb (kg) Fuel capacity U.S. gal (L) Volume-limit payload (pallets)** lb (kg) Design range (MTOW, volume-limit payload) nmi (km) Cruise Mach Takeoff field length (SL, 86 F, MTOW) ft (m) Initial cruise altitude (MTOW) ft (m) Landing field length (MLW) ft (m) Approach speed (MLW) kn Fuel consumption at volume-limit payload 500 nmi lb (kg) 1,000 nmi lb (kg) Typical mission rules * Boeing-equivalent thrust ** Volume-limit payload based on 9-lb/ft 3 cargo density and 7-lb/ft 3 bulk density Basic PW ,600/ ,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) ,950 (2,728) 35,900 (10,940) 5,100 (1,555) ,264 (4,656) 18,308 (8,305) Maximum PW ,100/ ,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) ,700 (2,347) 35,400 (10,790) 5,100 (1,555) ,264 (4,656) 18,308 (8,305)
14 F performance summary Rolls-Royce Engines Engines Takeoff thrust* lb/ F Main deck cargo 88- x 125-in pallets Lower hold cargo Bulk ft 3 (m 3 ) Maximum taxi weight lb (kg) Maximum takeoff weight lb (kg) Maximum landing weight lb (kg) Maximum zero fuel weight lb (kg) Operating empty weight (includes 3,300-lb tare) lb (kg) Fuel capacity U.S. gal (L) Volume-limit payload (pallets)** lb (kg) Design range (MTOW, volume-limit payload) nmi (km) Cruise Mach Takeoff field length (SL, 86 F, MTOW) ft (m) Initial cruise altitude (MTOW) ft (m) Landing field length (MLW) ft (m) Approach speed (MLW) kn Fuel consumption at volume-limit payload 500 nmi lb (kg) 1,000 nmi lb (kg) Typical mission rules * Boeing-equivalent thrust ** Volume-limit payload based on 9-lb/ft 3 cargo density and 7-lb/ft 3 bulk density Basic RB E4 40,200/ ,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) ,100 (2,164) 36,100 (11,000) 4,950 (1,510) ,875 (4,933) 19,355 (8,780) Maximum RB E4-B 43,500/ ,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) ,900 (2,103) 35,700 (10,880) 4,950 (1,510) ,875 (4,933) 19,355 (8,780)
15 F payload-range capability Pratt & Whitney Engines (50) (40) Payload, 1,000 lb (1,000 kg) ,000-lb (115,660-kg) MTOW 250,000-lb (113,400-kg) MTOW (30) 60 Volume limit payload (pallets) (20) 40 Fuel capacity U.S. gal (L) 11,276 (42,680 ) (10) 20 (0) Typical mission rules 200-nmi alternate 6.7 lb per U.S. gal fuel density (0) (2) (4) (6) (8) (10) Range, 1,000 nmi (1,000 km)
16 F payload-range capability Rolls-Royce engines Payload, 1,000 lb (1,000 kg) 120 (50) (40) ,000-lb (115,660-kg) MTOW 250,000-lb (113,400-kg) MTOW (30) 60 Volume limit payload (pallets) (20) 40 Fuel capacity U.S. gal (L) 11,276 (42,660) (10) 20 (0) Typical mission rules 200-nmi alternate 6.7 lb per U.S. gal fuel density (0) (2) (4) (6) (8) (10) Range, 1,000 nmi (1,000 km)
17 Mission profile Typical mission rules Mission Reserves Long-range cruise (LRC) LRC 100 nmi 200 nmi Block time and fuel Typical reserves Standard day Fuel density, 6.7 lb per U.S. gal Nominal performance Climbto1,50ft;acelto250kn Climbto10,0ftat250kn Aceleratetoclimbsped Climb Descendto10,0ft Decelerateto250kn Descendto1,50ft Aproachandland(5min) Taxin(5min)fromreserves 5%mision fuelalowance Misedaproach (Vtoclimbspedat1,50ft) AP Climb Descendto1,50ft Aproachandland(5min) Aproachold(30minat1,50ft) Taxi out (9 min) Takeoff (to 35 ft) Climb to 1,500 ft; accel to 250 kn Climb to 10,000 ft at 250 kn Accelerate to climb speed 5% mission fuel allowance Missed approach (V to climb speed at 1,500 ft) Climb Descend to 1,500 ft Approach and land (5 min) Climb Decelerate to 250 kn Descend to 1,500 ft Approach and land (5 min) Taxi in (5 min) from reserves Approach hold (30 min at 1,500 ft) Descend to 10,000 ft Still air range
18 Range capability from Los Angeles Volume limit payload Freighter 255,000-lb (115,660-kg) MTOW Anchorage Freighter 250,000-lb (113,400-kg) MTOW Juneau Seattle Chicago Montreal New York Bermuda Honolulu LOS ANGELES Mexico City Miami 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
19 Range capability from New York Volume limit payload Freighter 255,000-lb (115,660-kg) MTOW Freighter 250,000-lb (113,400-kg) MTOW Juneau Seattle Los Angeles Reykjavik NEW YORK London Terceira Madrid Miami Mexico 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 Panama City Quito Belem
20 Range capability from Miami Volume limit payload Freighter 255,000-lb (115,660-kg) MTOW Seattle Freighter 250,000-lb (113,400-kg) MTOW Chicago Los Angeles Montreal New York Terceira MIAMI Mexico City Panama City Caracas Bogota Quito Belem 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 Lima
21 Range capability from London Volume limit payload Freighter 255,000-lb (115,660-kg) MTOW Freighter 250,000-lb (113,400-kg) MTOW Gander Reykjavik Stockholm LONDON Moscow Baku Ashgabat Terceira Madrid Athens Bahrain Cairo Jeddah Dubai Khartoum PW2037/2040 engines Typical mission rules Airways and traffic allowances included Nominal performance 85% annual winds 3,300-lb (1,500-kg) tare weight Dakar Abidjan Lagos Ndjamena
22 Range capability from Singapore Volume limit payload Freighter 255,000-lb (115,660-kg) MTOW Freighter 250,000-lb (113,400-kg) MTOW Karachi Kabul Delhi Mumbai Colombo Calcutta Beijing Hong Kong Manila SINGAPORE Tokyo Guam Port Moresby Darwin PW2037/2040 engines Typical mission rules Airways and traffic allowances included Nominal performance 85% annual winds 3,300-lb (1,500-kg) tare weight Perth
23 Range capability from Tokyo Volume limit payload Freighter 255,000-lb (115,660-kg) MTOW Anchorage Freighter 250,000-lb (113,400-kg) MTOW Beijing Chengdu Kunming Ulaanbaatar Hong Kong Bangkok Manila Davao Vladivostok Seoul TOKYO Guam PW2037/2040 engines Typical mission rules Airways and traffic allowances included Nominal performance 85% annual winds 3,300-lb (1,500-kg) tare weight Port Moresby
24 757 Flight Deck 1/22/2008
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