User:C933103/test
| 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] | |
- ^ "Commercial Aircraft of the World" (PDF). Flight. 23 November 1961.
- ^ a b c "Airplane Characteristics for Airport Planning" (PDF). Boeing. 1989.
- ^ "A340-200 Specifications". Airbus.
- ^ "A340-300 Specifications". Airbus.
- ^ a b c d e "Aircraft Characteristics Airport Planning - A340-200/300" (PDF). Airbus. January 2016.
- ^ a b Cite error: The named reference
tcdswas invoked but never defined (see the help page). - ^ a b "Airbus Aircraft Data File". Civil Jet Aircraft Design. Elsevier. July 1999.
- ^ a b "A340-200/300". Aircraft Technical Data & Specifications. Airliners.net.
- ^ "Airbus A340-300" (PDF). Lufthansa. August 2010.
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