Airbus A380-800 with Engine Alliance GP7200-class engines

All geometry and textures are generated in code at load time. The page uses no 3D model files and no images.

DIMENSIONS
The overall layout follows the Airbus A380 Aircraft Characteristics – Airport and Maintenance Planning document (Nov 2012). It covers length, span, height, the fuselage, wing and tail outlines, door stations and sill heights, gear stations and the tyre sizes (1400×530R23 main, 1270×455R22 nose). Wing and tail outlines were traced from its general-arrangement drawings.

ENGINE
The engine is a two-spool, 1-5-9-2-6 layout with a 24-blade, 2.96 m swept fan. Data are from EASA TCDS IM.E.026: 100% N1 = 2,467 rpm, 100% N2 = 10,998 rpm, takeoff EGT limit 1,002 °C. Thrust reversers are fitted to the inboard engines only. Fuel flows are from the ICAO emissions databank. The fan-cowl doors open on their pylon hinges to show the fan-case accessories: the gearbox at 6 o'clock with starter, generator, hydraulic and fuel pumps, plus the engine controller, oil tank and harnesses. On the core there is the variable-stator linkage, fuel manifold, bleed ducts and clearance-control rings.

APPROXIMATIONS
Airfoil sections, the cockpit window outline, internal blade counts beyond those published, flap/slat angles per CONF (0/0, 20/0, 20/8, 20/17, 23/26, 23/33°), the start-sequence timing, the idle EGT and the under-cowl dressing (accessory positions, tube and harness routing) are representative of the engine class, not OEM data. The livery is a plain neutral scheme with no airline or manufacturer marks. Rotation playback is slowed by default so the blades don't alias. This is an educational visualisation, not a certified engineering model.

CONTROLS
Drag to orbit, scroll or pinch to zoom, right-drag or two-finger drag to pan. The control panel has engines, flight controls, lights, time of day, camera views, a cinematic tour of the aircraft and a film about the engine.