Comparison of Ilyushin Il-96 400 and Lockheed L-1011 TriStar 500

Attribute	Ilyushin Il-96 400 ×	Lockheed L-1011 TriStar 500 ×
General
Manufacturer	Ilyushin	Lockheed Martin Aeronautics
Model	Ilyushin Il-96 400	Lockheed L-1011 TriStar 500
Country	Russia	United States
Manufactured from (year)	1992	1968
Manufactured to (year)	-	1984
Type	Jumbo Passenger Jets	Mid Size Passenger Jets
Icao	IL96	L101
Performance
Engine	4x Aviadvigatel PS90-A1	3x 3 x Rolls-Royce RB.211-524B
Power, lbf (lbf)	38,326	50,000
Max cruise speed (km/h)	869	972
Travel range (km)	10,001	9,906
Fuel economy (km/l)	-	0.059
Service ceiling (m)	13,106	13,106
Rate of climb (m/sec)	-	14.33
Take off distance (m)	2,700	2,426
Landing distance (m)	1,650	1,734
Weights
Max take off weight (kg)	265,000	231,332
Max payload (kg)	58,000	42,003
Fuel tank capacity (l)	152,635	119,778
Baggage volume (m³)	-	420
Dimensions
Seats	436	246
Seats - business class	-	253
Seats - first class	-	234
Cabin height (m)	2.86	2.4
Cabin width (m)	5.7	5.8
Cabin length (m)	44.4	41.4
Exterior length (m)	63.9	50.05
Tail height (m)	15.7	16.8
Fuselage diameter (m)	6.08	6
Wing span (m)	60.1	50.1
Wing tips	Canted Winglets	No Winglets