|
Developing Nation: |
United States. |
|
First Flight(s): |
- L-1011-1
:
November 16, 1970,
N1011.
- L-1011-50
:
-
L-1011-100: April 25, 1975.
-
L-1011-150:
-
L-1011-200: October 8, 1976.
-
L-1011-250: December 1986.
-
L-1011-500: October 16, 1978. |
|
Crew: |
All types: 3 flight crew |
|
Passengers: |
- L-1011-1
: max. 400 (all economy) 256 in
typical 2 class configuration.
- L-1011-50
: max. 400 (all economy) 256 in typical 2 class
configuration.
-
L-1011-100: max. 400 (all economy) 256
in typical 2 class configuration.
-
L-1011-150: max. 400 (all economy) 256
in typical 2 class configuration.
-
L-1011-200: max. 400 (all economy) 256
in typical 2 class configuration.
-
L-1011-250: max. 400 (all economy) 256
in typical 2 class configuration.
-
L-1011-500: max. 330 (all economy) 246
in typical 2 class configuration (24 premium 222
economy class). |
| In
Service since: |
April 1972 (TWA). |
|
Wing Span: |
- L-1011-1
: 47,34 m.
- L-1011-50
: 47,34 m.
-
L-1011-100: 47,34 m.
-
L-1011-150: 47,34 m.
-
L-1011-200: 47,34 m.
-
L-1011-250: 47,34 m.
-
L-1011-500: 50,06 m. |
|
Wing Area: |
- L-1011-1
: 320 m².
- L-1011-50
: 320 m².
-
L-1011-100: 320 m².
-
L-1011-150: 320 m².
-
L-1011-200: 320 m².
-
L-1011-250: 320 m².
-
L-1011-500: 329 m². |
|
Length: |
- L-1011-1
: 54,17 m.
- L-1011-50
: 54,17 m.
-
L-1011-100: 54,17 m.
-
L-1011-150: 54,17 m.
-
L-1011-200: 54,17 m.
-
L-1011-250: 54,17 m.
-
L-1011-500: 50,05 m. |
|
Height: |
- All types: 16,87 m. |
|
Engine(s): |
- L-1011-1
: 3x 187 kN (42.000 lb) Rolls Royce RB211-22B
turbofans.
- L-1011-50
: 3x 187 kN (42.000 lb) Rolls Royce RB211-22B
turbofans.
-
L-1011-100: 3x 187 kN (42.000 lb) Rolls
Royce RB211-22B turbofans.
-
L-1011-150: 3x 187 kN (42.000 lb) Rolls
Royce RB211-22B turbofans.
-
L-1011-200: 3x 215 kN (48.000 lb) Rolls
Royce RB211-524 turbofans.
-
L-1011-250: 3x 215 kN (48.000 lb) Rolls
Royce RB211-524 turbofans.
-
L-1011-500: 3x 215 kN (48.000 lb) Rolls
Royce RB211-524B turbofans. |
|
Empty operating Weight: |
- L-1011-1 :
109.045 kg.
- L-1011-50 :
109.045 kg.
- L-1011-100:
109.045 kg.
- L-1011-150:
109.045 kg.
- L-1011-200:
112.670 kg.
- L-1011-250:
112.670 kg.
- L-1011-500:
111.310 kg. |
|
Max. Take off weight: |
- L-1011-1 :
195.045 kg.
- L-1011-50 :
195.045 kg.
- L-1011-100:
195.045 kg.
- L-1011-150:
195.045 kg.
- L-1011-200:
211.375 kg.
- L-1011-250:
211.375 kg.
- L-1011-500:
231.330 kg. |
|
Cruise Speed: |
- L-1011-1 :
890 km/h.
- L-1011-50 :
890 km/h.
- L-1011-100:
890 km/h.
- L-1011-150:
890 km/h.
- L-1011-200:
890 km/h.
- L-1011-250:
890 km/h.
- L-1011-500:
894 km/h. |
|
Max. Speed: |
- L-1011-1 :
973 km/h.
- L-1011-50 :
973 km/h.
- L-1011-100:
973 km/h.
- L-1011-150:
973 km/h.
- L-1011-200:
973 km/h.
- L-1011-250:
973 km/h.
- L-1011-500:
960 km/h. |
|
Operating altitude: |
All types: 10.058 m. |
|
Max. Range: |
- L-1011-1 :
5.760 km.
- L-1011-50 :
5.760 km.
- L-1011-100:
5.760 km.
- L-1011-150:
5.760 km.
- L-1011-200:
6.820 km.
- L-1011-250:
6.820 km.
- L-1011-500:
9.905 km. |
|
Total Production: |
- L-1011-1 / 50 /
100 / 150 / 200 / 250:
200x standard fuselage length.
- L-1011-500:
50x were sold when
production stopped in 1984. |
