Airbus 380 Profile

Airbus 380

Airbus 380 manufactured by Airbus S.A.S. is a two-level plane, with four engines are able to carry 850 passengers in a single-class configuration or 555 passengers in three class configuration. This Airbus 380 aircraft is also the largest commercial aircraft ever made ??(called superjumbo).

Airbus 380 Profile
National origin : Multi-national
Manufacturer : Airbus
Role : Wide-body, double-deck jet airliner
First flight :27 April 2005
Introduced : 25 October 2007 with Singapore Airlines
Primary users : Emirates, Singapore Airlines, Qantas, Lufthansa
Produced : 2004–present
Unit cost US$375.3 million

This Airbus 380 aircraft has four engines made ??by Rolls-Royce engine Trent-900 capable of delivering 36,280 pounds of thrust or four-engine turbo-fan Engine Alliance GP 7200 (a General Electric joint venture with Pratt & Whitney), with 37,003 kg of thrust.

The Airbus 380 has the standard version of the 854 seats for passengers, while the A380-900 has 1000 seats for passengers. above this plane there are shopping center, children’s playground, and other facilities.

Airbus 380 Specifications

Airbus 380 Measurement A380-800 A380-800F
Airbus 380 Cockpit crew Two
Airbus 380 Seating capacity 525 (3-class)
644 (2-class)
853 (1-class)
12 couriers
Length overall 72.73 m (238.6 ft)
Wingspan 79.75 m (261.6 ft)
Height 24.45 m (80.2 ft)
Wheelbase 33.58 m (110.2 ft) wing landing gear
36.85 m (120.9 ft) body landing gear
Wheel track 12.46 m (40.9 ft)
Outside fuselage width 7.14 m (23.4 ft)
Outside fuselage height 8.41 m (27.6 ft)
Maximum cabin width 6.58 m (21.6 ft) Main deck
5.92 m (19.4 ft) Upper deck (floor level)
Cabin length 49.9 m (164 ft) Main deck
44.93 m (147.4 ft) Upper deck
Wing area 845 m2 (9,100 sq ft)
Aspect ratio 7.5
Wing sweep 33.5°
Maximum taxi/ramp weight 571,000 kg (1,260,000 lb) 592,000 kg (1,310,000 lb)
Maximum take-off weight 569,000 kg (1,250,000 lb) 590,000 kg (1,300,000 lb)
Maximum landing weight 391,000 kg (860,000 lb) 427,000 kg (940,000 lb)
Maximum zero fuel weight 366,000 kg (810,000 lb) 402,000 kg (890,000 lb)
Typical Operating empty weight 276,800 kg (610,000 lb) 252,200 kg (556,000 lb)
Maximum structural payload 89,200 kg (197,000 lb) 149,800 kg (330,000 lb)
Maximum cargo volume 176 m3 (6,200 cu ft) 1,134 m3 (40,000 cu ft)
Maximum operating speed
at cruise altitude
Mach 0.89
(945 km/h, 587 mph, 510 knots)
Maximum design speed
in dive at cruise altitude
Mach 0.96
(at cruise altitude: 1020 km/h, 634 mph, 551 knots)
Take off run at MTOW/SL ISA 2,750 m (9,020 ft) 2,900 m (9,500 ft)
Range at design load 15,400 km (8,300 nmi, 9,500 mi) 10,400 km (5,600 nmi, 6,400 mi)
Service ceiling 13,115 m (43,028 ft)
Maximum fuel capacity 323,546 L
(85,472 US gal)
310,000 L
(81,893 US gal),
323,546 L
(85,472 US gal) option
Engines (4 x) GP7270 (A380-861)
Trent 970/B (A380-841)
Trent 972/B (A380-842)
GP7277 (A380-863F)
Trent 977/B (A380-843F)
Thrust (4 x) 311 kN (70,000 lbf) – 355 kN (80,000 lbf)
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