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Home / World commercial aircraft / Lockheed L-1011 TriStar

Lockheed L-1011 TriStar

First flight year — 1970

Lockheed L-1011 TriStar

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Lockheed L-1011 TriStar Specifications


L-1011-100L-1011-250L-1011-500
Dimensions
Length (m)54.254.250.0
Wingspan (m)47.347.350.0
Height (m)16.916.916.9
Wing area (m2)320320329
Weight
Maximum take-off weight (kg)211 380231 330231 500
Maximum landing weight (kg)166 920166 920166 920
Operating empty weight (kg)111 670113 400111 300
Maximum zero fuel weight (kg)153 310153 310153 310
Maximum payload (kg)41 60039 90042 000
Standard fuel capacity (litres)100 100119 900119 900
Performance
Range with max payload (km)7 0009 4009 900
Maximum operating altitude (m)12 80012 80012 800
Take-off field length (m)3 3003 0002 600
Landing field length (m) 1 8002 0002 100
EnginesR-R RB211-22B,
3 x 42020 lb
R-R RB211-524B4,
3 x 50000 lb
R-R RB211-524B4,
3 x 50000 lb
Cabin Data
Passengers (1-class)400362315
Passengers (2-class)310310250
Passengers (3-class)280280233
Cabin width (m)5.775.775.77


Typical Cabin Configuration of Lockheed L-1011 TriStar





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