A B C D E F G H I J K L M N O P Q R S T U V W X Y Z Misc
Lockheed L-1011 | L-1011-1 | L-1011-200 | L-1011-500 | | Description |
|---|
| Type | Widebody Jet Airliner |
|---|
| Passengers | 273 | 304 | 244 |
|---|
| First flight | November 16, 1970 | | October 16, 1978 |
|---|
| Manufacturer | Lockheed-California Co. |
|---|
| Dimensions |
|---|
| Length | 177 ft 8 in (54.2 m) | 177 ft 8 in (54.2 m) | 164 ft 2 in (50.0 m) |
|---|
| Wingspan | 155 ft 4 in (47.3 m) | 155 ft 4 in (47.3 m) | 164 ft 4 in (50.1 m) |
|---|
| Tailspan | 71 ft 7 in (21.8 m) | 71 ft 7 in (21.8 m) | 71 ft 7 in (21.8 m) |
|---|
| Height | 55 ft 4 in (16.7 m) | 55 ft 4 in (16.7 m) | 55 ft 4 in (16.7 m) |
|---|
| Wing area | 3456 ft² (321.1 m²) | 3456 ft² (321.1 m²) | 3541 ft² (329.0 m²) |
|---|
| Weights |
|---|
| Empty weight | 224,579 lb (101,867 kg) | 231,600 lb (105,052 kg) | 232,749 lb (105,573 kg) |
|---|
| Max. takeoff weight | 430,000 lb (195,000 kg) | 466,000 lb (209,000 kg) | 496,000 lb (225,000 kg) |
|---|
| Max. payload | 84,393 lb (38,280 kg) | 89,400 lb (40,551 kg) | 89,718 lb (40,695 kg) |
|---|
| Powerplant |
|---|
| Engine | 3 Rolls-Royce RB.211-22 B | 3 Rolls-Royce RB.211-524B | 3 Rolls-Royce RB.211-524B |
|---|
| Thrust | 42,000 lbf (187,000 kg) | 50,000 lbf (220,000 kg) | 50,000 lbf (220,000 kg) |
|---|
| Performance |
|---|
| Cruise speed | 495 mph (796 km/h) | 484 mph (779 km/h) | 484 mph (779 km/h) |
|---|
| Range | 4,610 mi (7,419 km) | 4,610 mi (7,419 km) | 6,340 mi (10,200 km) |
|---|
| Cruise altitude | 33,650 ft (10,260 m) | 34,000 ft (10,360 m) | 33,000 ft (10,060 m) |
|---|
| Service ceiling | 35,000 ft (10,670 m) | 36,000 ft (10,970 m) | 35,000 ft (10,670 m) |
|---|
* Yenne, Bill, Lockheed. Crescent Books, 1987. | Orthographically projected diagram of the Lockheed L-1011. |
{{aircontent *McDonnell Douglas DC-10
*Airbus A330-200
*Boeing 767-400ER>lists=
* List of Lockheed aircraft
* List of airliners
* List of active United Kingdom military aircraft
| |
