Airbus A340: Difference between revisions

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==Airbus A340-200==
==Airbus A340-200==
==Airbus A340-300==
==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 A340-500==
==Airbus A340-600==
==Airbus A340-600==
A340-600 SPECIFICATIONS
AIRCRAFT DIMENSIONS
metric imperial
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 (geometric) 63.45 m. 208 ft. 2 in.
Wing area (reference) 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
metric imperial
Engines RR Trent 500 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
Metric imperial
Maximum ramp weight 369.2 (381.2)
tonnes 813.9 (840.4)
lbs. x 1000
Maximum takeoff weight 368 (380)
tonnes 811.3 (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


==Specifications==
==Specifications==

Latest revision as of 18:16, 24 December 2009

Airbus A340 at a Glance
Role Widebody Jetliner
Country of Origin Fance
Manufacturer Airbus
Status In Production
Number Built 368
Unit Cost 186,000,000v$-210,000,000v$
File:Airplanes-Airbus A340.jpg

Airbus A340-200

Airbus A340-300

Airbus A340-500

Airbus A340-600

Specifications

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