Specifications
| Model | 200 | 300/400 | 475 | 500 |
|---|---|---|---|---|
| Source | ||||
| Cockpit crew | 2 | |||
| Seating capacity | 79 | 89 | 119 | |
| Length | 93 ft 6 in (28.50 m) | 107 ft 0 in (32.61 m) | ||
| Wingspan | 88 ft 6 in (26.97 m) | 93 ft 6 in (28.50 m) | ||
| Wing area | 980 sq ft (91 m2) | 1,031 sq ft (95.8 m2) | ||
| Height | 24 ft 6 in (7.47 m) | |||
| Cabin Width | 10 ft 6 in (3.20 m) | |||
| Cabin length | 50 ft 0 in (15.24 m) | 56 ft 10 in (17.32 m) | 70 ft 4 in (21.44 m) | |
| Typical empty weight | 46,312 lb (21,007 kg) | 48,722 lb (22,100 kg) | 51,731 lb (23,465 kg) | 54,582 lb (24,758 kg) |
| Maximum take-off weight | 78,500 lb (35,600 kg) | 87,000 lb (39,000 kg) | 98,500 lb (44,700 kg) | 104,500 lb (47,400 kg) |
| Maximum landing weight | 69,000 lb (31,000 kg) | 78,000 lb (35,000 kg) | 87,000 lb (39,000 kg) | |
| Maximum payload | 17,688 lb (8,023 kg) | 22,278 lb (10,105 kg) | 21,269 lb (9,647 kg) | 26,418 lb (11,983 kg) |
| Maximum cruising speed at 21,000 ft (6,400 m) |
548 mph (476 kn; 882 km/h) | 541 mph (470 kn; 871 km/h) | ||
| Stall speed | 124 mph (108 kn; 200 km/h) | 131 mph (114 kn; 211 km/h) | 114 mph (99 kn; 183 km/h) EAS | 121 mph (105 kn; 195 km/h) |
| Service ceiling | 35,000 ft (11,000 m) | |||
| Rate of climb | 2,750 ft/min (14.0 m/s) | 2,450 ft/min (12.4 m/s) | 2,480 ft/min (12.6 m/s) | 2,280 ft/min (11.6 m/s) |
| Takeoff run at MTOW | 6,250 ft (1,910 m) | 6,700 ft (2,000 m) | 5,500 ft (1,700 m) | 6,500 ft (2,000 m) |
| Range (Typical payload, 2 hr reserve) |
830 mi (720 nmi; 1,340 km) | 1,270 mi (1,100 nmi; 2,040 km) | 1,865 mi (1,621 nmi; 3,001 km) | 1,705 mi (1,482 nmi; 2,744 km) |
| Engine (x 2) | Rolls-Royce RB.163 Spey Mk 506 |
Rolls-Royce RB.163 Spey Mk 511 |
Rolls-Royce RB.163 Spey Mk 512-14DW |
|
| Max. thrust (x 2) | 10,410 lbf (46.3 kN) | 11,400 lbf (51 kN) | 12,550 lbf (55.8 kN) | |
Read more about this topic: BAC One-Eleven