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AIRBUS A340 WorldOfAirplane.com App Book Cafe Directory

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AIRBUS A340

The Airbus A340 is a long-range, wide-body passenger Aeroplane designed and manufactured by Airbus. Airbus imagined various versions of the A300, its first aircraft, in the mid-1970s, and built the A340 quadjet alongside the A330 twinjet.

The Airbus A340 is a twin-aisle passenger aircraft with four turbofan jet engines that was the first long-range Airbus. It was created using technology features such as the A320 glass cockpit; it shares many components with the A330, including identical fly-by-wire control systems and wings. The four engine design avoids ETOPS requirements such as increased inspection frequency

The A340 features a low cantilever wing; the A340-200/300 wing is nearly identical to that of the A330, with both engine pylons employed, although the A330 only uses the inboard one. The two engines for each wing give a more evenly distributed weight as well as a more outboard engine weight.




The first A340, a 200, was delivered to Lufthansa on February 2, 1993, and went into service on March 15, 1993. The aeroplane with 228 seats was called Nürnberg.On February 26, Air France received the 1000th Airbus A340-300, the first of nine anticipated to be operational by the end of the year. Air France replaced its Boeing 747s with A340s on its four-times-weekly Paris–Washington D.C. service. Lufthansa planned to replace aged DC-10s on Frankfurt–New York flights with A340s.



The A340 employs a modified A320 glass cockpit with side-stick controls rather than a traditional yoke. Six screens dominate the primary instrument panel, originally cathode ray tube monitors and eventually liquid crystal displays.The Electronic Flight Instrument System (EFIS) directs flight information, whereas the Electronic Centralised Aircraft Monitor directs system information (ECAM).



The aircraft monitors multiple sensors and informs the crew if any parameters are outside of their typical range; pilots may also analyse specific systems. Instead of paper instructions, electronic manuals are utilised, with optional web-based updates. Maintenance difficulties and expense were cut in half compared to the previous and smaller Airbus A310.Improved engine control and monitoring resulted in more time on the wing. The centralised maintenance computer can send real-time data to ground facilities.Heavy maintenance, such as structural upgrades, remained intact, but cabin sophistication, such as in-flight entertainment, was improved over previous airliners.

The A340 features a low cantilever wing; the A340-200/300 wing is nearly identical to that of the A330, with both engine pylons employed, although the A330 only uses the inboard one. The two engines for each wing offer a more evenly distributed weight, as well as a more outboard engine weight for a lower wing root bending moment at equal TOW, allowing a higher wing limitation MTOW for greater range. BAe designed and built the wings, which featured a long, narrow wing with a high aspect ratio for increased aerodynamic performance.



Specifications

Variant

A340-200

A340-300

A340-500

A340-600

Cockpit crew

Two

3-class seats

210–250

250–290

270–310

320–370

typ. layout

303 (30F + 273Y)

335 (30F + 305Y)

313 (12F + 36J + 265Y)

380 (12F + 54J + 314Y)

Exit limit

420/375

375/440

375

440

Length

59.39 m / 194 ft 10 in

63.66 m / 208 ft 10 in

67.33 m / 220 ft 11 in

74.77 m / 245 ft 3 in

Wingspan

60.3 m / 197.83 ft

63.45 m / 208.17 ft

Wing

363.1 m2 (3,908 sq ft), 29.7° sweep, 10 AR

437.3 m2 (4,707 sq ft), 31.1° sweep, 9.2 AR

Height

17.03 m / 55.86 ft

16.99 m / 55.72 ft

17.53 m / 57.51 ft

17.93 m / 58.84 ft

Fuselage

5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width

Cargo volume

158.4 m3 (5,590 cu ft)

132.4 m3 (4,680 cu ft)

149.7 m3 (5,290 cu ft)

201.7 m3 (7,120 cu ft)

MTOW

275 t (606,000 lb)

276.5 t (610,000 lb)

380 t (840,000 lb)

Max. PL

51 t (112,000 lb)

52 t (115,000 lb)

54 t (119,000 lb)

66 t (146,000 lb)<

OEW

118 t (260,000 lb)

131 t (289,000 lb)

168 t (370,000 lb)

174 t (384,000 lb)

Max. Fuel

110.4 t / 243,395 lb

175.2 t / 386,292 lb

155.5 t / 342,905 lb 

Engines (×4)

CFM International CFM56-5C

Trent 553

Trent 556

Thrust (×4)

138.78–151.24 kN (31,200–34,000 lbf)

248.12–275.35 kN (55,780–61,902 lbf)

Speed


Mach 0.86 (493 kn; 914 km/h) max,Mach 0.82 (470 kn; 871 km/h) cruise

Range, 3-class

12,400 km / 6,700 nmi

13,500 km / 7,300 nmi

16,670 km / 9,000 nmi

14,450 km / 7,800 nmi

Take off

2,900 m (9,500 ft)

3,000 m (10,000 ft)

3,350 m (10,990 ft)

3,400 m (11,200 ft)

Ceiling

41 100 ft (12 527 m)

41 450 ft (12 634 m)












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