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Model -50/-55[1] -61/71[2] -62/72[2] -63/73[2]
Passengers 189 259 189 259
max cargo (ft3) 1,390 2,500 1,615 2,500
Freighter cargo (ft3) -50: 9310
-55: 9,020
12,171 9,737 12,830
Freighter payload (lb) -50: 88,022
-55: 92,770
-61: 88,494
-71: 81,300
-62: 91,440
-72: 90,800
-63: 119,670
-73: 111,800
Wingspan (ft) 142.4 148.4
Length (ft) 150.7 187.4 157.5 187.4
fuselage width outside : 147 in (373.4 cm), inside : 138.25 in (351.2 cm)
MTOW (lb) -50: 315,000
-55: 325,000
325,000
-F: 328,000
350,000
-72F : 335,000
355,000
MLW (lb) 240,000[citation needed] -63: 258,000
-73: 275,000
Freighter MLW 240,000 258,000 250,000 275,000
MZFW (lb) -50: 176,500
-55: 190,000
224,000 195,000 -63: 230,000
-73: 231,000
Freighter MZFW 224,000 234,000 -62: 230,000
-72: 231,000
261,000
OEW (lb) -50: 124,800
-55: 138,266
-61: 152,101
-71: 163,700
-62: 143,255
-72: 153,200
-63: 158,738
-73: 166,200
Freighter OEW -50: 130,207
-55: 131,230
-61: 145,506
-71: 152,700
-62: 138,560
-72: 140,200
-63: 141,330
-73: 149,200
max fuel 23,393 USgal 24,275 USgal
Engines P&W JT3D-3
turbofans
super 60: P&W JT3D-3B
super 70: CFM56-2
turbofans
Cruise Mach 0.82 (895 km/h; 556 mph)
Range (nm) -50: 5,855
-55: 4,700
-61: 3,200
-71: 3,500
-62: 5,200
-72: 5,300
-63: 4,000
-73: 4,500
Freighter Range
-55: 3,000
-61: 2,300
-71: 2,900
-62: 3,200
-72: 3,900
-63: 2,300
-73: 2,900
Model A340-200[3] A340-300[4]
Cockpit crew Two
Typical seats 261 (3-class) 277
Other seatings 228 (10F + 48J + 170Y)
303 (30F + 273Y)[5]
335 (30F + 305Y)[5]
Exit limit[6] 375/420[a] 375/440[a]
Length 59.40 m (194 ft 11 in) 63.69 m (208 ft 11 in)
Wingspan 60.30 m (197 ft 10 in)
Wing area 363.1 m2 (3,908 sq ft)[7]
Wing sweep 29.7°[7]
Height 16.80 m (55 ft 1 in) 16.91 m (55 ft 6 in)
Cabin width 5.28 m (17 ft 4 in)
Fuselage width 5.64 m (18 ft 6 in)
Cargo volume 162.8 m3 (5,750 cu ft)
Maximum takeoff weight (MTOW) 275 t (606,000 lb) 276.5 t (610,000 lb)
Maximum landing weight (MLW) 181 t (399,000 lb) 192 t (423,000 lb)
Maximum zero fuel weight (MZFW) 169 t (373,000 lb) 183 t (403,000 lb)
Operating empty weight 126 t (278,000 lb)[8] 129.8 t (286,000 lb)[8]
Fuel capacity 155,040 L (40,960 US gal) 147,850 L (39,060 US gal)
Engines (×4) CFM International CFM56-5C
Thrust (×4)[6] 13,878–15,124 daN (31,200–34,000 lbf)
Cruise speed Mach 0.82 (871 km/h; 541 mph)[5]
Maximum speed Mach 0.86 (914 km/h; 568 mph)
Typical range 6,700 nmi (12,400 km) 7,300 nmi (13,500 km)
Take off (MTOW, SL, ISA) 2,900 m (9,500 ft)[5] 3,000 m (10,000 ft)[5]
Ceiling 12,500 m (41,000 ft)[9]
  1. ^ "Commercial Aircraft of the World" (PDF). Flight. 23 November 1961.
  2. ^ a b c "Airplane Characteristics for Airport Planning" (PDF). Boeing. 1989.
  3. ^ "A340-200 Specifications". Airbus.
  4. ^ "A340-300 Specifications". Airbus.
  5. ^ a b c d e "Aircraft Characteristics Airport Planning - A340-200/300" (PDF). Airbus. January 2016.
  6. ^ a b Cite error: The named reference tcds was invoked but never defined (see the help page).
  7. ^ a b "Airbus Aircraft Data File". Civil Jet Aircraft Design. Elsevier. July 1999.
  8. ^ a b "A340-200/300". Aircraft Technical Data & Specifications. Airliners.net.
  9. ^ "Airbus A340-300" (PDF). Lufthansa. August 2010.


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