Airbus A340 - Revision history

Alasizon: Protected "Airbus A340" [edit=autoconfirmed:move=autoconfirmed]

2009-12-24T18:16:52Z

Protected "Airbus A340" [edit=autoconfirmed:move=autoconfirmed]

← Older revision	Revision as of 18:16, 24 December 2009
(No difference)

Alasizon: /* Airbus A340-300 */

2009-09-11T23:36:21Z

Airbus A340-300

@@ Line 13: / Line 13: @@
 ==Airbus A340-200==
 ==Airbus A340-300==
 ==Airbus A340-500==

Alasizon: /* Airbus A340-600 */

2009-09-11T23:36:07Z

Airbus A340-600

@@ Line 65: / Line 65: @@
 ==Airbus A340-500==
 ==Airbus A340-600==
 ==Specifications==

Alasizon: /* Specifications */

2009-09-11T23:35:50Z

Specifications

← Older revision		Revision as of 23:35, 11 September 2009
Line 115:		Line 115:

	==Specifications==		==Specifications==
			{\|
			\|- bgcolor="#DDDD"
			!Measurement
			! A340-200
			! A340-300
			! A340-500/-500HGW
			! A340-600/-600HGW
			\|- bgcolor="#EEEEEE"
			\|Cockpit crew \|\| colspan="4" align="center" \| Two
			\|- bgcolor="#EEEEEE"
			\|Seating capacity \|\| align="center" \| 239 (3-class) \|\| align="center" \| 295 (3-class) \|\| align="center" \| 313 (3-class) \|\| align="center" \| 380 (3-class)
			\|- bgcolor="#EEEEEE"
			\|Length \|\| align="center" \| 59.39 m<br>194 ft 10 in \|\| align="center" \| 63.60 m<br>208 ft 8 in \|\| align="center" \| 67.90 m<br>222 ft 9 in \|\| align="center" \| 75.30 m<br>247 ft 0 in
			\|- bgcolor="#EEEEEE"
			\|Wingspan \|\| colspan="2" align="center" \| 60.30 m<br>197 ft 10 in \|\| colspan="2" align="center" \|63.45 m<br>208 ft 2 in
			\|- bgcolor="#EEEEEE"
			\|Wing area \|\| colspan="2" align="center" \| 361.6 m²<br>3,892 ft² \|\| colspan="2" align="center" \| 439 m²<br>4,725 ft²
			\|- bgcolor="#EEEEEE"
			\|Wing sweepback \|\| colspan="2" align="center" \| 30° \|\| colspan="2" align="center" \|31.1°
			\|- bgcolor="#EEEEEE"
			\|Height \|\| align="center" \| 16.70 m<br>54 ft 9 in \|\| align="center" \| 16.85 m<br>55 ft 3 in \|\| align="center" \| 17.10 m<br>56 ft 1 in \|\| align="center" \| 17.30 m<br>56 ft 9 in
			\|- bgcolor="#EEEEEE"
			\|Cabin width \|\| colspan="4" align="center" \| 5.28 m (17.3 ft)
			\|- bgcolor="#EEEEEE"
			\|Fuselage width \|\| colspan="4" align="center" \| 5.64 m (18.5 ft)
			\|- bgcolor="#EEEEEE"
			\|Wheelbase \|\| align="center" \| 23.24 m<br>76 ft 3 in \|\| align="center" \|25.60 m<br>84 ft 0 in \|\| align="center" \| 27.59 m<br>90 ft 6 in \|\| align="center" \| 32.89 m<br>107 ft 11 in
			\|- bgcolor="#EEEEEE"
			\|Typical empty weight \|\| align="center" \| 129,000 kg<br>284,396 lb \|\| align="center" \| 129,275 kg<br>295,503 lb \|\| align="center" \| 170,400 kg<br>375,668 lb\|\| align="center" \| 177,000 kg<br>390,218 lb
			\|- bgcolor="#EEEEEE"
			\|Maximum take-off weight \|\| align="center" \| 275,000 kg<br>606,300 lb \|\| align="center" \| 276,500 kg<br>609,600 lb \|\| align="center" \| 372,000/380,000 kg<br>820,100 /837,800 lb \|\| align="center" \| 368,000/380,000 kg<br>811,300/837,800 lb
			\|- bgcolor="#EEEEEE"
			\|Cruising speed \|\| colspan="2" align="center" \| Mach 0.82 (896 km/h, 484 knots, 557 mph \|\| colspan="2" align="center" \| Mach 0.83 (907 km/h, 490 knots, 564 mph)
			\|- bgcolor="#EEEEEE"
			\|Take off run at MTOW \|\| align="center" \| 2,990 m<br>9,810 ft \|\| align="center" \| 3,000 m<br>9,840 ft \|\| align="center" \| 3,050 m<br>10,000 ft \|\| align="center" \| 3,100 m<br>10,170 ft
			\|- bgcolor="#EEEEEE"
			\|Range fully loaded \|\| align="center" \| 14,800 km 8,000 NM \|\| align="center" \| 13,700 km 7,400 NM \|\| align="center" \| 16,020/16,700 km 8,650/9,000 NM \|\| align="center" \| 14,360/14,630 km 7,750/7,900 NM
			\|- bgcolor="#EEEEEE"
			\|Max. fuel capacity \|\| align="center" \| 155,040 L 40,957 gal \|\| align="center" \| 140,640 L 37,153 gal \|\| align="center" \| 214,810/222,000 L 56,750/58,646 gal \|\| align="center" \|195,881/204,500 L 51,746/54,023 gal
			\|- bgcolor="#EEEEEE"
			\|Cargo capacity \|\| align="center" \| 18 LD3s/6 pallets \|\| align="center" \| 30 LD3s/10 pallets \|\| align="center" \| 32 LD3s/11 pallets \|\| align="center" \|42 LD3s/14 pallets
			\|- bgcolor="#EEEEEE"
			\|Service ceiling \|\| colspan="4" align="center" \| 11,887 m<br>39,000 ft
			\|- bgcolor="#EEEEEE"
			\|Engines (4x) \|\| align="center" \| CFM56-5C2 (138.78 kN)<br>CFM56-5C3 (144.57 kN)<br>CFM56-5C4 (151.25 kN) \|\| align="center" \| CFM56-5C2 (138.78 kN)<br>CFM56-5C3 (144.57 kN)<br>CFM56-5C4 (151.25 kN)<br>CFM56-5C4P (149.9 kN) \|\| align="center" \|Rolls-Royce Trent <br> 553/556 (236/249 kN) \|\| align="center" \| Trent 556/560 (249/260 kN)
			\|}
	[[Category:Widebody Jetliners]]		[[Category:Widebody Jetliners]]

124.182.214.29: /* Airbus A340-600 */

2009-09-11T06:30:15Z

Airbus A340-600

@@ Line 65: / Line 65: @@
 ==Airbus A340-500==
 ==Airbus A340-600==
 ==Specifications==
 [[Category:Widebody Jetliners]]

124.182.214.29: /* Airbus A340-300 */

2009-09-11T06:29:53Z

Airbus A340-300

New page

{{Infobox Aircraft Type
|type= [[:Category:Widebody Jetliners|Widebody Jetliner]]
|country= Fance
|manufacturer= Airbus
|status= In Production
|number built= 368
|unit cost= 186,000,000v$-210,000,000v$
|updateday= 10
|updatemonth=9
|updateyear= 2009
|picture= yes
}}
==Airbus A340-200==
==Airbus A340-300==
A340-300 SPECIFICATIONS
AIRCRAFT DIMENSIONS
metric imperial
Overall length 63.6 m. 208 ft. 10 in.
Height 16.85 m. 55 ft. 3 in.
Fuselage diameter 5.64 m. 18 ft. 6 in.
Maximum cabin width 5.28 m. 17 ft. 4 in.
Cabin length 50.35 m. 165 ft. 3 in.
Wingspan (geometric) 60.3 m. 197 ft. 10 in.
Wing area (reference) 361.6 m2 3,892 ft2
Wing sweep (25% chord) 30 degrees 30 degrees
Wheelbase 25.60 m. 84 ft.
Wheel track 10.69 m. 35 ft. 1 in.
BASIC OPERATING DATA
metric imperial
Engines four CFM56-
5C4/P four CFM56-
5C4/P
Engine thrust range 139-151 kN 31,200-34,000
lb. slst
Typical passenger seating 295 295
Range (w/max. passengers) 13,350
(13,700) km. 7,200 (7,400)
nm.
Max. operating Mach number (Mmo) 0.86 Mo. 0.86 Mo.
Bulk hold volume - Standard/option 19.7 / 13.76 m3 695 / 486 ft3
DESIGN WEIGHTS
metric imperial
Maximum ramp weight 275.9 (277.4)
tonnes 608.3 (611.5)
lbs. x 1000
Maximum takeoff weight 275 (276.5)
tonnes 606.0 (609.6)
lbs. x 1000
Maximum landing weight 190 (192)
tonnes 418.9 (423.3)
lbs. x 1000
Maximum zero fuel weight 178 (181)
tonnes 392.4 (399) lbs.
x 1000
Maximum fuel capacity 140,640
(147,850) Litres 37,150 (39,060)
US gal.
Typical operating weight empty 129.3 (130.2)
tonnes 285 (287) lbs. x
1000
Typical volumetric payload 43.5 (41)
tonnes 95.9 (90.5) lbs.
x 1000

==Airbus A340-500==
==Airbus A340-600==
==Specifications==
[[Category:Widebody Jetliners]]