1. AVIATION

2. RESEARCH ON AIRBUS A-300 AND A-380

9. Measurement A380-800 A380-800F Cockpit crew Two Seating capacity 525 (3-class) [7] 644 (2-class) 853 (1-class) 12 couriers Length 73 m (239 ft 6 in ) Span 79.8 m (261 ft 10 in) Height 24.1 m (79 ft 1 in) Wheelbase 30.4 m (99 ft 8 in) Outside fuselage width 7.14 m (23 ft 6 in) Cabin width, main deck 6.60 m (21 ft 8 in) Cabin width, upper deck 5.94 m (19 ft 6 in) Wing area 845 m² (9,100 sq ft) Operating empty weight 276,800 kg (610,200 lb ) 252,200 kg (556,000 lb) Maximum take-off weight 560,000 kg (1,235,000 lb) 590,000 kg (1,300,000 lb) Maximum payload 90,800 kg (200,000 lb) 152,400 kg (336,000 lb) Cruising speed Mach 0.85 Maximum speed Mach 0.89 Take off run at MTOW 2,750 m (9,020 ft) [77] 2,900 m (9,510 ft) [77] Range at design load 15,200 km (8,200 nmi ) 10,400 km (5,600 nmi) Service ceiling 13,115 m (43,000 ft) Maximum fuel capacity 310,000 L (81,890 US gal ) 310,000 L (81,890 US gal), 356,000 L (94,000 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)

11. ADVANTAGES AND DISADVANTAGES OF THE CURRENT SCENARIO IN THE AVIATION INDUSTRIES

13. THE COMPARISION ON THE LATEST TECHNOLOGY OF AIRBUS A-300 AND A-380