Airbus A340: Difference between revisions

From FSAirlinesWiki
Jump to navigation Jump to search
 
m Protected "Airbus A340" [edit=autoconfirmed:move=autoconfirmed]
 
(4 intermediate revisions by 2 users not shown)
Line 13: Line 13:
==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==
==Specifications==
==Specifications==
{|
|- bgcolor="#DDDD"
!Measurement
! A340-200
! A340-300
! A340-500/-500HGW
! A340-600/-600HGW
|- bgcolor="#EEEEEE"
|Cockpit crew || colspan="4" align="center" |  Two
|- bgcolor="#EEEEEE"
|Seating capacity || align="center" | 239 (3-class) || align="center" | 295 (3-class) || align="center" | 313 (3-class) || align="center" | 380 (3-class)
|- bgcolor="#EEEEEE"
|Length || align="center" | 59.39&nbsp;m<br>194&nbsp;ft 10&nbsp;in  || align="center" | 63.60&nbsp;m<br>208&nbsp;ft 8&nbsp;in  || align="center" | 67.90&nbsp;m<br>222&nbsp;ft 9&nbsp;in || align="center" | 75.30&nbsp;m<br>247&nbsp;ft 0&nbsp;in
|- bgcolor="#EEEEEE"
|Wingspan || colspan="2" align="center" | 60.30&nbsp;m<br>197&nbsp;ft 10&nbsp;in || colspan="2" align="center" |63.45&nbsp;m<br>208&nbsp;ft 2&nbsp;in
|- bgcolor="#EEEEEE"
|Wing area || colspan="2" align="center" | 361.6 m²<br>3,892&nbsp;ft² || colspan="2" align="center" | 439 m²<br>4,725&nbsp;ft²
|- bgcolor="#EEEEEE"
|Wing sweepback || colspan="2" align="center" | 30° || colspan="2" align="center" |31.1°
|- bgcolor="#EEEEEE"
|Height || align="center" | 16.70&nbsp;m<br>54&nbsp;ft 9&nbsp;in  || align="center" | 16.85&nbsp;m<br>55&nbsp;ft 3&nbsp;in  || align="center" | 17.10&nbsp;m<br>56&nbsp;ft 1&nbsp;in  || align="center" | 17.30&nbsp;m<br>56&nbsp;ft 9&nbsp;in
|- bgcolor="#EEEEEE"
|Cabin width || colspan="4" align="center" | 5.28&nbsp;m (17.3&nbsp;ft)
|- bgcolor="#EEEEEE"
|Fuselage width || colspan="4" align="center" | 5.64&nbsp;m (18.5&nbsp;ft)
|- bgcolor="#EEEEEE"
|Wheelbase || align="center" | 23.24&nbsp;m<br>76&nbsp;ft 3&nbsp;in || align="center" |25.60&nbsp;m<br>84&nbsp;ft 0&nbsp;in || align="center" | 27.59&nbsp;m<br>90&nbsp;ft 6&nbsp;in || align="center" | 32.89&nbsp;m<br>107&nbsp;ft 11&nbsp;in
|- bgcolor="#EEEEEE"
|Typical empty weight || align="center" | 129,000&nbsp;kg<br>284,396&nbsp;lb || align="center" | 129,275&nbsp;kg<br>295,503&nbsp;lb || align="center" | 170,400&nbsp;kg<br>375,668&nbsp;lb|| align="center" | 177,000&nbsp;kg<br>390,218&nbsp;lb
|- bgcolor="#EEEEEE"
|Maximum take-off weight || align="center" | 275,000&nbsp;kg<br>606,300&nbsp;lb || align="center" | 276,500&nbsp;kg<br>609,600&nbsp;lb || align="center" | 372,000/380,000&nbsp;kg<br>820,100 /837,800&nbsp;lb || align="center" | 368,000/380,000&nbsp;kg<br>811,300/837,800&nbsp;lb
|- bgcolor="#EEEEEE"
|Cruising speed || colspan="2" align="center" | Mach 0.82 (896&nbsp;km/h, 484&nbsp;knots, 557&nbsp;mph || colspan="2" align="center"  | Mach 0.83 (907&nbsp;km/h, 490&nbsp;knots, 564&nbsp;mph)
|- bgcolor="#EEEEEE"
|Take off run at MTOW || align="center" | 2,990&nbsp;m<br>9,810&nbsp;ft || align="center" | 3,000&nbsp;m<br>9,840&nbsp;ft || align="center" | 3,050&nbsp;m<br>10,000&nbsp;ft || align="center" | 3,100&nbsp;m<br>10,170&nbsp;ft
|- bgcolor="#EEEEEE"
|Range fully loaded || align="center" | 14,800&nbsp;km 8,000&nbsp;NM || align="center" | 13,700&nbsp;km 7,400&nbsp;NM || align="center" | 16,020/16,700&nbsp;km 8,650/9,000&nbsp;NM || align="center" | 14,360/14,630&nbsp;km 7,750/7,900&nbsp;NM
|- bgcolor="#EEEEEE"
|Max. fuel capacity || align="center" | 155,040&nbsp;L 40,957&nbsp;gal || align="center" | 140,640&nbsp;L 37,153&nbsp;gal || align="center" | 214,810/222,000&nbsp;L 56,750/58,646&nbsp;gal || align="center" |195,881/204,500&nbsp;L 51,746/54,023&nbsp;gal
|- bgcolor="#EEEEEE"
|Cargo capacity || align="center" | 18 LD3s/6 pallets  || align="center" | 30 LD3s/10 pallets  || align="center" | 32 LD3s/11 pallets  || align="center" |42 LD3s/14 pallets
|- bgcolor="#EEEEEE"
|Service ceiling || colspan="4" align="center" | 11,887&nbsp;m<br>39,000&nbsp;ft
|- bgcolor="#EEEEEE"
|Engines (4x) || align="center" | CFM56-5C2 (138.78&nbsp;kN)<br>CFM56-5C3 (144.57&nbsp;kN)<br>CFM56-5C4 (151.25&nbsp;kN) || align="center" | CFM56-5C2 (138.78&nbsp;kN)<br>CFM56-5C3 (144.57&nbsp;kN)<br>CFM56-5C4 (151.25&nbsp;kN)<br>CFM56-5C4P (149.9&nbsp;kN) || align="center" |Rolls-Royce Trent <br> 553/556 (236/249&nbsp;kN) || align="center" | Trent 556/560 (249/260&nbsp;kN)
|}
[[Category:Widebody Jetliners]]
[[Category:Widebody Jetliners]]

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)