Airbus A340

Metric

Imperial

AIRCRAFT DIMENSIONS

Overall length

59.39 m.

194 ft. 10 in.

Height

16.7 m.

54 ft. 9 in.

Fuselage diameter

5.64 m.

18 ft. 6 in.

Maximum cabin width

5.28 m.

17 ft. 4 in.

Cabin length

46.06 m.

165 ft 3 in.

Wingspan

60.3 m.

197 ft. 10 in.

Wing area

361.6 m2

3,892 ft2.

Wing sweep (25% chord)

30 degrees

30 degrees

Wheelbase

23.24 m.

76 ft. 3 in.

Wheel track

10.69 m.

35 ft. 1 in.

BASIC OPERATING DATA

Engines

four CFM56-5C4

four CFM56-5C4

Engine thrust range

139-151 kN

31,200-34,000 lb. slst

Typical passenger seating

239

239

Range (w/max. passengers)

14,800 km.

8,000 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

Maximum ramp weight

275.9 tonnes

608.2 lbs. x 1000

Maximum takeoff weight

275 tonnes

606.3 lbs. x 1000

Maximum landing weight

185 tonnes

407.9 lbs. x 1000

Maximum zero fuel weight

173 tonnes

381.4 lbs. x 1000

Maximum fuel capacity

155,040 Litres

40,960 US gal.

Typical operating weight empty

43.5 tonnes

95.9 lbs. X 1000

Typical volumetric payload

30.8 tonnes

67.9 lbs. x 100

Metric

Imperial

AIRCRAFT DIMENSIONS

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

60.3 m.

197 ft. 10 in.

Wing area

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

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

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

Metric

Imperial

AIRCRAFT DIMENSIONS

Overall length

67.9 m.

222 ft. 8 in.

Height

17.1 m.

56 ft. 1 in.

Fuselage diameter

5.64 m.

18 ft. 6 in.

Maximum cabin width

5.28 m.

17 ft. 4 in.

Cabin length

53.56 m.

175 ft. 9 in.

Wingspan

63.45 m.

208 ft. 2 in.

Wing area

439.4 m2

4,729 ft2

Wing sweep (25% chord)

31.1 degrees

31.1 degrees

Wheelbase

27.59 m.

90 ft. 6 in.

Wheel track

10.69 m.

35 ft. 1 in.

BASIC OPERATING DATA

Engines

four RR Trent 500

four RR Trent 500

Engine thrust range

236 (249) kN

53,000 (56,000) lb. slst

Typical passenger seating

313 (3-class)

313 (3-class)

Range (w/max. passengers)

16,100 (16,700) km.

8,670 (9,000) 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

Maximum ramp weight

373.2 (381.2) tonnes

822.8 (840.4) lbs. x 1000

Maximum takeoff weight

372 (380) tonnes

820.1 (837.8) lbs. x 1000

Maximum landing weight

243 (246) tonnes

535.7 (542.3) lbs. x 1000

Maximum zero fuel weight

230 (232) tonnes

507.1 (511.5) lbs. x 1000

Maximum fuel capacity

214,810 (222,000) Litres

56,750 (58,646) US gal.

Typical operating weight empty

170.9 (174.8) tonnes

376.8 (385.4) lbs. x 1000

Typical volumetric payload

43.3 tonnes

95.5 lbs. x 1000

Metric

Imperial

AIRCRAFT DIMENSIONS

Overall length

75.3 m.

247 ft. 1 in.

Height

17.3 m.

56 ft. 9 in.

Fuselage diameter

5.64 m.

18 ft. 6 in.

Maximum cabin width

5.28 m.

17 ft. 4 in.

Cabin length

60.98 m.

200 ft. 1 in.

Wingspan

63.45 m.

208 ft. 2 in.

Wing area

439.4 m2

4,729 ft2

Wing sweep (25% chord)

31.1 degrees

31.1 degrees

Wheelbase

32.89 m.

107 ft. 11 in.

Wheel track

10.69 m.

35 ft. 1 in.

BASIC OPERATING DATA

Engines

four RR Trent 500

four RR Trent 500

Engine thrust range

249 (267) kN

56,000 (60,000) lb. slst

Typical passenger seating

380

380

Range (w/max. passengers)

14,360 (14,600) km.

7,750 (7,900) 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

Maximum ramp weight

369.2 (381.2) tonnes

813.9 (840.4) lbs. x 1000

Maximum takeoff weight

372 (380) tonnes

820.1 (837.8) lbs. x 1000

Maximum landing weight

259 (265) tonnes

571 (584.2) lbs. x 1000

Maximum zero fuel weight

245 (251) tonnes

540.1 (553.4) lbs. x 1000

Maximum fuel capacity

195,881 (204,500) Litres

51,746 (54,023.2) US gal.

Typical operating weight empty

177.8 (181.9) tonnes

392.0 (400.9) lbs. x 1000

Typical volumetric payload

55.6 tonnes

122.6 lbs. x 1000