Difference between revisions of "Airbus A340"
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==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 m<br>194 ft 10 in || align="center" | 63.60 m<br>208 ft 8 in || align="center" | 67.90 m<br>222 ft 9 in || align="center" | 75.30 m<br>247 ft 0 in | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Wingspan || colspan="2" align="center" | 60.30 m<br>197 ft 10 in || colspan="2" align="center" |63.45 m<br>208 ft 2 in | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Wing area || colspan="2" align="center" | 361.6 m²<br>3,892 ft² || colspan="2" align="center" | 439 m²<br>4,725 ft² | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Wing sweepback || colspan="2" align="center" | 30° || colspan="2" align="center" |31.1° | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Height || align="center" | 16.70 m<br>54 ft 9 in || align="center" | 16.85 m<br>55 ft 3 in || align="center" | 17.10 m<br>56 ft 1 in || align="center" | 17.30 m<br>56 ft 9 in | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Cabin width || colspan="4" align="center" | 5.28 m (17.3 ft) | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Fuselage width || colspan="4" align="center" | 5.64 m (18.5 ft) | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Wheelbase || align="center" | 23.24 m<br>76 ft 3 in || align="center" |25.60 m<br>84 ft 0 in || align="center" | 27.59 m<br>90 ft 6 in || align="center" | 32.89 m<br>107 ft 11 in | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Typical empty weight || align="center" | 129,000 kg<br>284,396 lb || align="center" | 129,275 kg<br>295,503 lb || align="center" | 170,400 kg<br>375,668 lb|| align="center" | 177,000 kg<br>390,218 lb | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Maximum take-off weight || align="center" | 275,000 kg<br>606,300 lb || align="center" | 276,500 kg<br>609,600 lb || align="center" | 372,000/380,000 kg<br>820,100 /837,800 lb || align="center" | 368,000/380,000 kg<br>811,300/837,800 lb | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Cruising speed || colspan="2" align="center" | Mach 0.82 (896 km/h, 484 knots, 557 mph || colspan="2" align="center" | Mach 0.83 (907 km/h, 490 knots, 564 mph) | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Take off run at MTOW || align="center" | 2,990 m<br>9,810 ft || align="center" | 3,000 m<br>9,840 ft || align="center" | 3,050 m<br>10,000 ft || align="center" | 3,100 m<br>10,170 ft | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Range fully loaded || align="center" | 14,800 km 8,000 NM || align="center" | 13,700 km 7,400 NM || align="center" | 16,020/16,700 km 8,650/9,000 NM || align="center" | 14,360/14,630 km 7,750/7,900 NM | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Max. fuel capacity || align="center" | 155,040 L 40,957 gal || align="center" | 140,640 L 37,153 gal || align="center" | 214,810/222,000 L 56,750/58,646 gal || align="center" |195,881/204,500 L 51,746/54,023 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 m<br>39,000 ft | ||
| + | |- bgcolor="#EEEEEE" | ||
| + | |Engines (4x) || align="center" | CFM56-5C2 (138.78 kN)<br>CFM56-5C3 (144.57 kN)<br>CFM56-5C4 (151.25 kN) || align="center" | CFM56-5C2 (138.78 kN)<br>CFM56-5C3 (144.57 kN)<br>CFM56-5C4 (151.25 kN)<br>CFM56-5C4P (149.9 kN) || align="center" |Rolls-Royce Trent <br> 553/556 (236/249 kN) || align="center" | Trent 556/560 (249/260 kN) | ||
| + | |} | ||
[[Category:Widebody Jetliners]] | [[Category:Widebody Jetliners]] | ||
Revision as of 23:35, 11 September 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$-210,000,000v$ |
| 262px | |
Airbus A340-200
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 A340-600
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
| 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) |
