For those of you who asked about various A380 specifications, the following are various figures for A380-800 (the main pax version, as you know)...
Operating weight empty: 276,800 kg. (610,240 lb.)
MTOW: 560,000 kg. (1,234,580 lbs.)
Max. landing weight: 386,000 kg. (850,980 lb.)
Engines: four
RR Trent 970s or four Engine Alliance GP7270s (both 70,000 lb. thrust)
Takeoff field length: 2,987 m (9,800 ft.)
Max operating speed/economic cruise speed: Mach 0.89/0.85
Service ceiling: 42,980 ft. (13,100 m)
Typical range: 14,816 km (8,000 nm)
Wing span/length/height/wheel track: 79.56 m (261 ft. 4 in.)/72.75 m (238 ft. 8 in.)/24.08 m (79 ft. 9 in.)/14.33 m (47 ft. 0 in.)
Max cabin width upper/main deck: 5.92 m (19 ft. 5 in.)/6.58 m (21 ft. 7 in.)
Bulk/total hold volume: 18.4 cubic metres (650 cubic feet)/171.0 cubic metres (6,039 cubic feet)
Pax accomodation (nominal): 555
Landing gear arrangement: 1 X two-wheel nose gear, 2 X six-wheel main body bogies, 2 X four-wheel wing bogies
Other info: the A380 will be quieter and burn 20% less fuel per passenger than the 747.
Hope that helps. If any of you need specs for the A380-800F, I have those figures too. All of the above info is from the November 2003 issue of the U.K. publication "Air International".
qantasA332