Boeing 747 - Revision history

Alasizon: Protected "Boeing 747" [edit=autoconfirmed:move=autoconfirmed]

2009-12-24T18:26:17Z

Protected "Boeing 747" [edit=autoconfirmed:move=autoconfirmed]

← Older revision		Revision as of 18:26, 24 December 2009
Line 98:		Line 98:
	{\| style="text-align: center; font-size:95%;" class="wikitable"		{\| style="text-align: center; font-size:95%;" class="wikitable"
	\|-		\|-
	! \|\| 747-100 \|\| 747-200B \|\| 747-300 \|\| 747-400<br/>747-400ER \|\| 747-8I		! \|\| 747-100 \|\| 747-200B \|\| 747-300 \|\| 747-400<br/>747-400ER \|\| 747-8I \|\| 747SP
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Cockpit Crew \|\| colspan="3"\| Three \|\| colspan="2"\| Two		\|Cockpit Crew \|\| colspan="3"\| Three \|\| colspan="2"\| Two \|\| Three
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Typical seating capacity \|\| colspan="2" \|452 (2-class)<br/> 366 (3-class) \|\| 496 (2-class)<br/> 412 (3-class) \|\| 524 (2-class)<br/> 416 (3-class) \|\| 467 (3-class)		\|Typical seating capacity \|\| colspan="2" \|452 (2-class)<br/> 366 (3-class) \|\| 496 (2-class)<br/> 412 (3-class) \|\| 524 (2-class)<br/> 416 (3-class) \|\| 467 (3-class) \|\| 331 (28 first, 303 economy)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Length \|\| colspan="4" \| 231 ft 10 in (70.6 m)\|\| 250 ft 8 in (76.4 m)		\|Length \|\| colspan="4" \| 231 ft 10 in (70.6 m)\|\| 250 ft 8 in (76.4 m) \|\| 184 ft 9 in (56.31 m)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Wingspan \|\| colspan="3" \| 195 ft 8 in (59.6 m) \|\| 211 ft 5 in (64.4 m) \|\| 224 ft 7 in (68.5 m)		\|Wingspan \|\| colspan="3" \| 195 ft 8 in (59.6 m) \|\| 211 ft 5 in (64.4 m) \|\| 224 ft 7 in (68.5 m) \|\| 195 ft 8 in (59.64 m)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Tail height \|\| colspan="3" \| 63 ft 5 in (19.3 m) \|\| 63 ft 8 in (19.4 m) \|\| 63 ft 6 in (19.4 m)		\|Tail height \|\| colspan="3" \| 63 ft 5 in (19.3 m) \|\| 63 ft 8 in (19.4 m) \|\| 63 ft 6 in (19.4 m)\|\| 65 ft 10 in (20.06 m)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Weight empty \|\| 358,000 lb <br/> (162,400 kg) \|\| 383,000 lb <br/> (174,000 kg) \|\| 392,800 lb <br/> (178,100 kg) \|\| 393,263 lb <br/> (178,756 kg) <br />'''ER:''' 406,900 lb <br /> (184,600 kg) \|\| 472,900 lb <br /> (214,503 kg)		\|Weight empty \|\| 358,000 lb <br/> (162,400 kg) \|\| 383,000 lb <br/> (174,000 kg) \|\| 392,800 lb <br/> (178,100 kg) \|\| 393,263 lb <br/> (178,756 kg) <br />'''ER:''' 406,900 lb <br /> (184,600 kg) \|\| 472,900 lb <br /> (214,503 kg) \|\| 336,870 lb (152,780 kg)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Maximum takeoff weight \|\| 735,000 lb <br/> (333,390 kg) \|\| colspan="2" \| 833,000 lb <br/>(377,842 kg) \|\| 875,000 lb <br/> (396,890 kg) <br/> '''ER:''' 910,000 lb <br/> (412,775 kg) \|\| 975,000 lb <br/> (442,253 kg)		\|Maximum takeoff weight \|\| 735,000 lb <br/> (333,390 kg) \|\| colspan="2" \| 833,000 lb <br/>(377,842 kg) \|\| 875,000 lb <br/> (396,890 kg) <br/> '''ER:''' 910,000 lb <br/> (412,775 kg) \|\| 975,000 lb <br/> (442,253 kg) \|\| 670,000 lb (304,000 kg)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Cruising speed <br/>(at 35,000 ft altitude) \|\| colspan="3" \| Mach 0.84 <br/>(555 mph, 893 km/h, 481 knots ) \|\| Mach 0.85 <br/> (567 mph, 913 km/h, 493 kn) <br/>'''ER:''' Mach 0.855 <br/> (570 mph, 918 km/h, 495 kn)\|\| Mach 0.855 <br /> (570 mph, 918 km/h, 495 kn)		\|Cruising speed <br/>(at 35,000 ft altitude) \|\| colspan="3" \| Mach 0.84 <br/>(555 mph, 893 km/h, 481 knots ) \|\| Mach 0.85 <br/> (567 mph, 913 km/h, 493 kn) <br/>'''ER:''' Mach 0.855 <br/> (570 mph, 918 km/h, 495 kn)\|\| Mach 0.855 <br /> (570 mph, 918 km/h, 495 kn) \|\| .88 Mach (535 knots, 990 km/h)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Maximum speed \|\| colspan="3" \| Mach 0.89 <br />(594 mph, 955 km/h, 516 kn) \|\| Mach 0.92 <br/> (614 mph, 988 km/h, 533 kn) \|\|		\|Maximum speed \|\| colspan="3" \| Mach 0.89 <br />(594 mph, 955 km/h, 516 kn) \|\| Mach 0.92 <br/> (614 mph, 988 km/h, 533 kn) \|\| Mach 0.92 (614 mph, 533 kn, 988 km/h) \|\| 0.92 Mach (591 knots, 1,095 km/h)
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Required runway at MTOW* \|\| colspan="2" \| 10,466 ft (3,190 m) \|\| 10,893 ft (3,320 m) \|\| 9,902 ft (3,018 m) <br/>'''ER:''' 10,138 ft (3,090 m) \|\| 10,138 ft (3,090 m)		\|Required runway at MTOW* \|\| colspan="2" \| 10,466 ft (3,190 m) \|\| 10,893 ft (3,320 m) \|\| 9,902 ft (3,018 m) <br/>'''ER:''' 10,138 ft (3,090 m) \|\| 10,138 ft (3,090 m) \|\|
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Maximum range <br/>at MTOW\|\| 5,300 NM <br/> (9,800 km) \|\| 6,850 nmi <br/> (12,700 km) \|\| 6,700 nmi <br/> (12,400 km) \|\| 7,260 nmi <br/> (13,450 km) <br/>'''ER:''' 7,670 nmi <br/> (14,205 km) \|\| 8,000 nmi <br/> (14,815 km)		\|Maximum range <br/>at MTOW\|\| 5,300 NM <br/> (9,800 km) \|\| 6,850 nmi <br/> (12,700 km) \|\| 6,700 nmi <br/> (12,400 km) \|\| 7,260 nmi <br/> (13,450 km) <br/>'''ER:''' 7,670 nmi <br/> (14,205 km) \|\| 8,000 nmi <br/> (14,815 km) \|\| 6,650 nm (7,650 mi, 12,325 km) with 276 passengers
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Max. fuel capacity \|\| 48,445 U.S. gal <br /> (40,339 imp gal/183,380 L) \|\| colspan="2" \| 52,410 U.S. gal <br/>(43,640 imp gal/199,158 L) \|\| 57,285 U.S. gal <br /> (47,700 imp gal/216,840 L) <br/>'''ER:''' 63,705 U.S. gal <br/> (53,045 imp gal/241,140 L) \|\| 64,225 U.S. gal <br/> (53,478 imp gal/243,120 L)		\|Max. fuel capacity \|\| 48,445 U.S. gal <br /> (40,339 imp gal/183,380 L) \|\| colspan="2" \| 52,410 U.S. gal <br/>(43,640 imp gal/199,158 L) \|\| 57,285 U.S. gal <br /> (47,700 imp gal/216,840 L) <br/>'''ER:''' 63,705 U.S. gal <br/> (53,045 imp gal/241,140 L) \|\| 64,225 U.S. gal <br/> (53,478 imp gal/243,120 L) \|\|
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Engine models (x 4) \|\| PW JT9D-7A <br/> RR RB211-524B2 \|\| PW JT9D-7R4G2 <br/> GE CF6-50E2 <br/> RR RB211-524D4 \|\| PW JT9D-7R4G2 <br /> GE CF6-80C2B1 <br/> RR RB211-524D4 \|\| PW 4062 <br/> GE CF6-80C2B5F <br/> RR RB211-524G/H <br/>'''ER:''' GE CF6-80C2B5F \|\| GEnx-2B67		\|Engine models (x 4) \|\| PW JT9D-7A <br/> RR RB211-524B2 \|\| PW JT9D-7R4G2 <br/> GE CF6-50E2 <br/> RR RB211-524D4 \|\| PW JT9D-7R4G2 <br /> GE CF6-80C2B1 <br/> RR RB211-524D4 \|\| PW 4062 <br/> GE CF6-80C2B5F <br/> RR RB211-524G/H <br/>'''ER:''' GE CF6-80C2B5F \|\| GEnx-2B67 \|\| 4× Pratt & Whitney JT9D-7R4W turbofan engines
	\|- bgcolor="#EEEEEE"		\|- bgcolor="#EEEEEE"
	\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN)		\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN) \|\| 46,500 lbf (206.8 kN) each
	\|}		\|}

Alasizon at 03:02, 13 September 2009

2009-09-13T03:02:41Z

← Older revision		Revision as of 03:02, 13 September 2009
Line 93:		Line 93:

	Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.		Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.


	==Specifications==		==Specifications==
	~~=Specifications=~~
	{\| style="text-align: center; font-size:95%;" class="wikitable"		{\| style="text-align: center; font-size:95%;" class="wikitable"
	\|-		\|-

Alasizon: /* Boeing 747-400 Specific Specifications */

2009-09-13T03:02:01Z

Boeing 747-400 Specific Specifications

← Older revision		Revision as of 03:02, 13 September 2009
Line 94:		Line 94:
	Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.		Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.
	==Specifications==		==Specifications==
			=Specifications=
	{\| style="text-align: center; font-size:95%;" class="wikitable"		{\| style="text-align: center; font-size:95%;" class="wikitable"
	\|-		\|-
	! ~~Measurement~~ \|\| 747-100 \|\| 747-200B \|\| 747-300 \|\| 747-400<br/>747-400ER \|\| 747-8I		! \|\| 747-100 \|\| 747-200B \|\| 747-300 \|\| 747-400<br/>747-400ER \|\| 747-8I
	\|-		\|- bgcolor="#EEEEEE"
	\|Cockpit Crew \|\| colspan="3"\| Three \|\| colspan="2"\| Two		\|Cockpit Crew \|\| colspan="3"\| Three \|\| colspan="2"\| Two
	\|-		\|- bgcolor="#EEEEEE"
	\|Typical seating capacity \|\| colspan="2" \|452 (2-class)<br/> 366 (3-class) \|\| 496 (2-class)<br/> 412 (3-class) \|\| 524 (2-class)<br/> 416 (3-class) \|\| 467 (3-class)		\|Typical seating capacity \|\| colspan="2" \|452 (2-class)<br/> 366 (3-class) \|\| 496 (2-class)<br/> 412 (3-class) \|\| 524 (2-class)<br/> 416 (3-class) \|\| 467 (3-class)
	\|-		\|- bgcolor="#EEEEEE"
	\|Length \|\| colspan="4" \| 231 ft 10 in (70.6 m)\|\| 250 ft 8 in (76.4 m)		\|Length \|\| colspan="4" \| 231 ft 10 in (70.6 m)\|\| 250 ft 8 in (76.4 m)
	\|-		\|- bgcolor="#EEEEEE"
	\|Wingspan \|\| colspan="3" \| 195 ft 8 in (59.6 m) \|\| 211 ft 5 in (64.4 m) \|\| 224 ft 7 in (68.5 m)		\|Wingspan \|\| colspan="3" \| 195 ft 8 in (59.6 m) \|\| 211 ft 5 in (64.4 m) \|\| 224 ft 7 in (68.5 m)
	\|-		\|- bgcolor="#EEEEEE"
	\|Tail height \|\| colspan="3" \| 63 ft 5 in (19.3 m) \|\| 63 ft 8 in (19.4 m) \|\| 63 ft 6 in (19.4 m)		\|Tail height \|\| colspan="3" \| 63 ft 5 in (19.3 m) \|\| 63 ft 8 in (19.4 m) \|\| 63 ft 6 in (19.4 m)
	\|-		\|- bgcolor="#EEEEEE"
	\|Weight empty \|\| 358,000 lb <br/> (162,400 kg) \|\| 383,000 lb <br/> (174,000 kg) \|\| 392,800 lb <br/> (178,100 kg) \|\| 393,263 lb <br/> (178,756 kg) <br />'''ER:''' 406,900 lb <br /> (184,600 kg) \|\| 472,900 lb <br /> (214,503 kg)		\|Weight empty \|\| 358,000 lb <br/> (162,400 kg) \|\| 383,000 lb <br/> (174,000 kg) \|\| 392,800 lb <br/> (178,100 kg) \|\| 393,263 lb <br/> (178,756 kg) <br />'''ER:''' 406,900 lb <br /> (184,600 kg) \|\| 472,900 lb <br /> (214,503 kg)
	\|-		\|- bgcolor="#EEEEEE"
	\|Maximum takeoff weight \|\| 735,000 lb <br/> (333,390 kg) \|\| colspan="2" \| 833,000 lb <br/>(377,842 kg) \|\| 875,000 lb <br/> (396,890 kg) <br/> '''ER:''' 910,000 lb <br/> (412,775 kg) \|\| 975,000 lb <br/> (442,253 kg)		\|Maximum takeoff weight \|\| 735,000 lb <br/> (333,390 kg) \|\| colspan="2" \| 833,000 lb <br/>(377,842 kg) \|\| 875,000 lb <br/> (396,890 kg) <br/> '''ER:''' 910,000 lb <br/> (412,775 kg) \|\| 975,000 lb <br/> (442,253 kg)
	\|-		\|- bgcolor="#EEEEEE"
	\|Cruising speed <br/>(at 35,000 ft altitude) \|\| colspan="3" \| Mach 0.84 <br/>(555 mph, 893 km/h, 481 knots ) \|\| Mach 0.85 <br/> (567 mph, 913 km/h, 493 kn) <br/>'''ER:''' Mach 0.855 <br/> (570 mph, 918 km/h, 495 kn)\|\| Mach 0.855 <br /> (570 mph, 918 km/h, 495 kn)		\|Cruising speed <br/>(at 35,000 ft altitude) \|\| colspan="3" \| Mach 0.84 <br/>(555 mph, 893 km/h, 481 knots ) \|\| Mach 0.85 <br/> (567 mph, 913 km/h, 493 kn) <br/>'''ER:''' Mach 0.855 <br/> (570 mph, 918 km/h, 495 kn)\|\| Mach 0.855 <br /> (570 mph, 918 km/h, 495 kn)
	\|-		\|- bgcolor="#EEEEEE"
	\|Maximum speed \|\| colspan="3" \| Mach 0.89 <br />(594 mph, 955 km/h, 516 kn) \|\| Mach 0.92 <br/> (614 mph, 988 km/h, 533 kn) \|\|		\|Maximum speed \|\| colspan="3" \| Mach 0.89 <br />(594 mph, 955 km/h, 516 kn) \|\| Mach 0.92 <br/> (614 mph, 988 km/h, 533 kn) \|\|
	\|-		\|- bgcolor="#EEEEEE"
	\|Required runway at MTOW* \|\| colspan="2" \| 10,466 ft (3,190 m) \|\| 10,893 ft (3,320 m) \|\| 9,902 ft (3,018 m) <br/>'''ER:''' 10,138 ft (3,090 m) \|\| 10,138 ft (3,090 m)		\|Required runway at MTOW* \|\| colspan="2" \| 10,466 ft (3,190 m) \|\| 10,893 ft (3,320 m) \|\| 9,902 ft (3,018 m) <br/>'''ER:''' 10,138 ft (3,090 m) \|\| 10,138 ft (3,090 m)
	\|-		\|- bgcolor="#EEEEEE"
	\|Maximum range <br/>at MTOW\|\| 5,300 NM <br/> (9,800 km) \|\| 6,850 nmi <br/> (12,700 km) \|\| 6,700 nmi <br/> (12,400 km) \|\| 7,260 nmi <br/> (13,450 km) <br/>'''ER:''' 7,670 nmi <br/> (14,205 km) \|\| 8,000 nmi <br/> (14,815 km)		\|Maximum range <br/>at MTOW\|\| 5,300 NM <br/> (9,800 km) \|\| 6,850 nmi <br/> (12,700 km) \|\| 6,700 nmi <br/> (12,400 km) \|\| 7,260 nmi <br/> (13,450 km) <br/>'''ER:''' 7,670 nmi <br/> (14,205 km) \|\| 8,000 nmi <br/> (14,815 km)
	\|-		\|- bgcolor="#EEEEEE"
	\|Max. fuel capacity \|\| 48,445 U.S. gal <br /> (40,339 imp gal/183,380 L) \|\| colspan="2" \| 52,410 U.S. gal <br/>(43,640 imp gal/199,158 L) \|\| 57,285 U.S. gal <br /> (47,700 imp gal/216,840 L) <br/>'''ER:''' 63,705 U.S. gal <br/> (53,045 imp gal/241,140 L) \|\| 64,225 U.S. gal <br/> (53,478 imp gal/243,120 L)		\|Max. fuel capacity \|\| 48,445 U.S. gal <br /> (40,339 imp gal/183,380 L) \|\| colspan="2" \| 52,410 U.S. gal <br/>(43,640 imp gal/199,158 L) \|\| 57,285 U.S. gal <br /> (47,700 imp gal/216,840 L) <br/>'''ER:''' 63,705 U.S. gal <br/> (53,045 imp gal/241,140 L) \|\| 64,225 U.S. gal <br/> (53,478 imp gal/243,120 L)
	\|-		\|- bgcolor="#EEEEEE"
	\|Engine models (x 4) \|\| PW JT9D-7A <br/> RR RB211-524B2 \|\| PW JT9D-7R4G2 <br/> GE CF6-50E2 <br/> RR RB211-524D4 \|\| PW JT9D-7R4G2 <br /> GE CF6-80C2B1 <br/> RR RB211-524D4 \|\| PW 4062 <br/> GE CF6-80C2B5F <br/> RR RB211-524G/H <br/>'''ER:''' GE CF6-80C2B5F \|\| GEnx-2B67		\|Engine models (x 4) \|\| PW JT9D-7A <br/> RR RB211-524B2 \|\| PW JT9D-7R4G2 <br/> GE CF6-50E2 <br/> RR RB211-524D4 \|\| PW JT9D-7R4G2 <br /> GE CF6-80C2B1 <br/> RR RB211-524D4 \|\| PW 4062 <br/> GE CF6-80C2B5F <br/> RR RB211-524G/H <br/>'''ER:''' GE CF6-80C2B5F \|\| GEnx-2B67
	\|-		\|- bgcolor="#EEEEEE"
	\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN)		\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN)
	\|}		\|}
	~~===Boeing 747-400 Specific Specifications===~~
	~~{\| float="left" clear="both" width="75%"~~
	\|-
	~~\|{{showhide\|title=Click <nowiki>[show]</nowiki> to expand\|width=auto\|content=~~
	~~{{:Boeing 747/400 Specs}}~~
	}}

Alasizon: /* Specifications */

2009-09-13T02:55:47Z

Specifications

← Older revision		Revision as of 02:55, 13 September 2009
Line 126:		Line 126:
	\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN)		\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN)
	\|}		\|}
			===Boeing 747-400 Specific Specifications===
			{\| float="left" clear="both" width="75%"
			\|-
			\|{{showhide\|title=Click <nowiki>[show]</nowiki> to expand\|width=auto\|content=
			{{:Boeing 747/400 Specs}}
			}}

Alasizon at 02:53, 13 September 2009

2009-09-13T02:53:29Z

Show changes

Alasizon: /* Specifications */

2009-09-13T02:52:00Z

Specifications

← Older revision		Revision as of 02:52, 13 September 2009
Line 93:		Line 93:

	Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.		Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.
			==Specifications==
			==Specifications==
			{\| style="text-align: center; font-size:95%;" class="wikitable"
			\|-
			! Measurement \|\| 747-100 \|\| 747-200B \|\| 747-300 \|\| 747-400<br/>747-400ER \|\| 747-8I
			\|-
			\|Cockpit Crew \|\| colspan="3"\| Three \|\| colspan="2"\| Two
			\|-
			\|Typical seating capacity \|\| colspan="2" \|452 (2-class)<br/> 366 (3-class) \|\| 496 (2-class)<br/> 412 (3-class) \|\| 524 (2-class)<br/> 416 (3-class) \|\| 467 (3-class)
			\|-
			\|Length \|\| colspan="4" \| 231 ft 10 in (70.6 m)\|\| 250 ft 8 in (76.4 m)
			\|-
			\|Wingspan \|\| colspan="3" \| 195 ft 8 in (59.6 m) \|\| 211 ft 5 in (64.4 m) \|\| 224 ft 7 in (68.5 m)
			\|-
			\|Tail height \|\| colspan="3" \| 63 ft 5 in (19.3 m) \|\| 63 ft 8 in (19.4 m) \|\| 63 ft 6 in (19.4 m)
			\|-
			\|Weight empty \|\| 358,000 lb <br/> (162,400 kg) \|\| 383,000 lb <br/> (174,000 kg) \|\| 392,800 lb <br/> (178,100 kg) \|\| 393,263 lb <br/> (178,756 kg) <br />'''ER:''' 406,900 lb <br /> (184,600 kg) \|\| 472,900 lb <br /> (214,503 kg)
			\|-
			\|Maximum takeoff weight \|\| 735,000 lb <br/> (333,390 kg) \|\| colspan="2" \| 833,000 lb <br/>(377,842 kg) \|\| 875,000 lb <br/> (396,890 kg) <br/> '''ER:''' 910,000 lb <br/> (412,775 kg) \|\| 975,000 lb <br/> (442,253 kg)
			\|-
			\|Cruising speed <br/>(at 35,000 ft altitude) \|\| colspan="3" \| Mach 0.84 <br/>(555 mph, 893 km/h, 481 knots ) \|\| Mach 0.85 <br/> (567 mph, 913 km/h, 493 kn) <br/>'''ER:''' Mach 0.855 <br/> (570 mph, 918 km/h, 495 kn)\|\| Mach 0.855 <br /> (570 mph, 918 km/h, 495 kn)
			\|-
			\|Maximum speed \|\| colspan="3" \| Mach 0.89 <br />(594 mph, 955 km/h, 516 kn) \|\| Mach 0.92 <br/> (614 mph, 988 km/h, 533 kn) \|\|
			\|-
			\|Required runway at MTOW* \|\| colspan="2" \| 10,466 ft (3,190 m) \|\| 10,893 ft (3,320 m) \|\| 9,902 ft (3,018 m) <br/>'''ER:''' 10,138 ft (3,090 m) \|\| 10,138 ft (3,090 m)
			\|-
			\|Maximum range <br/>at MTOW\|\| 5,300 NM <br/> (9,800 km) \|\| 6,850 nmi <br/> (12,700 km) \|\| 6,700 nmi <br/> (12,400 km) \|\| 7,260 nmi <br/> (13,450 km) <br/>'''ER:''' 7,670 nmi <br/> (14,205 km) \|\| 8,000 nmi <br/> (14,815 km)
			\|-
			\|Max. fuel capacity \|\| 48,445 U.S. gal <br /> (40,339 imp gal/183,380 L) \|\| colspan="2" \| 52,410 U.S. gal <br/>(43,640 imp gal/199,158 L) \|\| 57,285 U.S. gal <br /> (47,700 imp gal/216,840 L) <br/>'''ER:''' 63,705 U.S. gal <br/> (53,045 imp gal/241,140 L) \|\| 64,225 U.S. gal <br/> (53,478 imp gal/243,120 L)
			\|-
			\|Engine models (x 4) \|\| PW JT9D-7A <br/> RR RB211-524B2 \|\| PW JT9D-7R4G2 <br/> GE CF6-50E2 <br/> RR RB211-524D4 \|\| PW JT9D-7R4G2 <br /> GE CF6-80C2B1 <br/> RR RB211-524D4 \|\| PW 4062 <br/> GE CF6-80C2B5F <br/> RR RB211-524G/H <br/>'''ER:''' GE CF6-80C2B5F \|\| GEnx-2B67
			\|-
			\|Engine thrust (per engine) \|\| \| PW 46,500 lbf <br/>(207 kN) <br/> RR 50,100 lbf <br/>(223 kN)\|\| PW 54,750 lbf (244 kN) <br/> GE 52,500 lbf (234 kN) <br/> RR 53,000 lbf <br/>(236 kN) \|\| PW 54,750 lbf <br/>(244 kN) <br/> GE 55,640 lbf <br/>(247 kN) <br/> RR 53,000 lbf (236 kN) \|\| PW 63,300 lbf (282 kN)<br /> GE 62,100 lbf (276 kN) <br/> RR 59,500/60,600 lbf (265/270 kN) <br/>'''ER:''' GE 62,100 lbf <br/>(276 kN) \|\| 66,500 lbf <br/>(296 kN)
			\|}

Alasizon: /* Boeing 747-8F */

2009-09-13T02:44:36Z

Boeing 747-8F

← Older revision		Revision as of 02:44, 13 September 2009
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	==Boeing 747-8F==		==Boeing 747-8F==
	Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner~~. Artist's impression of a Boeing 747-8 Intercontinental in the colors of Lufthansa, the launch customer~~.		Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner.

	Offered is the 747-8 Freighter or 747-8F, which derives from the 747-400ERF. The 747-8F can accommodate 154 tons (140 tonnes) of cargo. To aid loading and unloading, it features an overhead nose-door. It has 16 percent more payload capacity than the 747-400F and can hold seven additional standard air cargo containers. The 747-8F is scheduled to enter service in 2009.		Offered is the 747-8 Freighter or 747-8F, which derives from the 747-400ERF. The 747-8F can accommodate 154 tons (140 tonnes) of cargo. To aid loading and unloading, it features an overhead nose-door. It has 16 percent more payload capacity than the 747-400F and can hold seven additional standard air cargo containers. The 747-8F is scheduled to enter service in 2009.

	Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.		Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.

Alasizon: /* Boeing 747-8I */

2009-09-13T02:44:20Z

Boeing 747-8I

← Older revision		Revision as of 02:44, 13 September 2009
Line 82:		Line 82:
	==Boeing 747-8I==		==Boeing 747-8I==
	Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner.		Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner.
	~~Artist's impression of a Boeing 747-8 Intercontinental in the colors of Lufthansa, the launch customer.~~

	The passenger version, dubbed 747-8 Intercontinental or 747-8I, will be able to carry up to 467 passengers in a 3-class configuration and fly more than 8,000 nmi (15,000 km) at Mach 0.855. As a derivative of the already common 747-400, the 747-8 has the economic benefit of similar training and interchangeable parts.[156] The 747-8I is scheduled to enter service in 2010.		The passenger version, dubbed 747-8 Intercontinental or 747-8I, will be able to carry up to 467 passengers in a 3-class configuration and fly more than 8,000 nmi (15,000 km) at Mach 0.855. As a derivative of the already common 747-400, the 747-8 has the economic benefit of similar training and interchangeable parts.[156] The 747-8I is scheduled to enter service in 2010.

Alasizon: /* Boeing 747-400ER */

2009-09-13T02:43:22Z

Boeing 747-400ER

← Older revision		Revision as of 02:43, 13 September 2009
Line 53:		Line 53:

	==Boeing 747-400ER==		==Boeing 747-400ER==
	The -~~400~~ was ~~offered in extended range~~ passenger (400ER). The 747-400ER ~~entered service~~ in ~~November 2002 with Qantas~~, the ~~only airline ever to order~~ the ~~passenger version~~.		The 747-400ER (Extended range) was launched on 28 November 2000 following an order by Qantas for 6 aircraft. This was ultimately the only order for the passenger version. The -400ER can fly an additional 805 km or carry 6,800 kg more freight. Qantas received the first -400ER on 31 October 2002.

			The 747-400ER includes the option of 1 or 2 additional 3,240 US gallon body fuel tanks in the forward cargo hold. Manufactured by Marshall Aerospace, these tanks utilize innovative metal to metal honeycomb bonded technology to achieve a high dry weight to fuel volume ratio. Similar technology has been used in the development by Marshall of body fuel tanks for the 777-200LR and P-8A Poseidon MMA aircraft.

	==Boeing 747-400D==		==Boeing 747-400D==
Line 80:		Line 82:
	==Boeing 747-8I==		==Boeing 747-8I==
	Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner.		Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner.
	Artist's impression of a Boeing 747-8 Intercontinental in the colors of Lufthansa, the launch customer		Artist's impression of a Boeing 747-8 Intercontinental in the colors of Lufthansa, the launch customer.

	The passenger version, dubbed 747-8 Intercontinental or 747-8I, will be able to carry up to 467 passengers in a 3-class configuration and fly more than 8,000 nmi (15,000 km) at Mach 0.855. As a derivative of the already common 747-400, the 747-8 has the economic benefit of similar training and interchangeable parts.[156] The 747-8I is scheduled to enter service in 2010.		The passenger version, dubbed 747-8 Intercontinental or 747-8I, will be able to carry up to 467 passengers in a 3-class configuration and fly more than 8,000 nmi (15,000 km) at Mach 0.855. As a derivative of the already common 747-400, the 747-8 has the economic benefit of similar training and interchangeable parts.[156] The 747-8I is scheduled to enter service in 2010.

	Several units are under construction at Boeing's Everett facility. The 747-8I has received 27 orders as of June 2009		Several units are under construction at Boeing's Everett facility. The 747-8I has received 27 orders as of June 2009.

	==Boeing 747-8F==		==Boeing 747-8F==
			Boeing announced a new 747 variant, the 747-8 (referred to as the 747 Advanced prior to launch) on 14 November 2005, which will use the same engine and cockpit technology as the 787, hence the use of the "8". Plans call for the new design to be quieter, more economical and more environmentally friendly. The 747-8 is stretched to add more payload capacity. This involves lengthening from 232 to 251 feet (70.8 to 76.4 m), surpassing the Airbus A340-600 to become the world's longest airliner. Artist's impression of a Boeing 747-8 Intercontinental in the colors of Lufthansa, the launch customer.

			Offered is the 747-8 Freighter or 747-8F, which derives from the 747-400ERF. The 747-8F can accommodate 154 tons (140 tonnes) of cargo. To aid loading and unloading, it features an overhead nose-door. It has 16 percent more payload capacity than the 747-400F and can hold seven additional standard air cargo containers. The 747-8F is scheduled to enter service in 2009.

			Several units are under construction at Boeing's Everett facility. The 747-8F has received 78 orders as of June 2009.

Alasizon: /* Boeing 747-400D */

2009-09-13T02:41:46Z

Boeing 747-400D

← Older revision		Revision as of 02:41, 13 September 2009
Line 56:		Line 56:

	==Boeing 747-400D==		==Boeing 747-400D==
	The -~~400 was offered in domestic~~ (~~400D~~)~~, which was built~~ for short ~~range operations~~ and ~~does not include~~ winglets, ~~however these can be retrofitted~~.		The 747-400D (Domestic) is a high density seating model developed for short-haul domestic Japanese flights. The aircraft is capable of seating a maximum of 568 passengers in a 2-class configuration or 660 passengers in a single-class configuration. The -400D lacks the wing tip extensions and winglets included on other variants. The benefits of winglets would be minimal on short routes. The -400D may be converted to the long range version when needed. The 747-400D is also unusual in having more windows on both sides of the upper deck than the basic -400 series (2 portside, 4 starboard).

			The 747-400 Domestic first flew on 18 March 1991 and entered service with Japan Airlines on 22 October 1991. The last was delivered to All Nippon Airways in December 1995.

	==Boeing 747-400M==		==Boeing 747-400M==