BAC 111-414EG Dan Air "1980s" Colors. G-AZED  
     
 
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 (1,900 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)

 

 
 

 

Role Short-range jetliner
Manufacturer British Aircraft Corporation
First flight 20 August 1963
Introduction 1965
Status Non-Operational service
Primary users British Airways
American Airlines
Braniff Airways
British United Airways
Produced 19631982 (United Kingdom)
19821989 (Romania)
Number built 244

 

   
     

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