Lockheed L-1011 TriStar
Airliner
The Lockheed L-1011 TriStar is a three-engine medium- to long-range widebody jet airliner for up to 400 passengers produced by the US-American manufacturer Lockheed Corporation.
The L-1011 TriStar 500 (L-1011-385-3) is a long-range variant with shortened fuselage (-4,11m / 13ft 6in) and a capacity of max. 315 passengers (typical 253). All other variants have a length of length 54,17m (177ft 8in) and a capacity of max. 400 passengers (typical 234). The TriStar was Lockheed's last commercial aircraft.
Crew | 3 | |
Passengers | 256-400 (246-315) |
Propulsion | 3 Turbofan Engines | |
Engine Model | Rolls-Royce RB.211-22C-02 | |
Engine Power (each) | 182,4 kN | 41000 lbf |
alternative Engine Variant | ||
Engine Model | Rolls-Royce RB.211-524B4-02 | |
Engine Power (each) | 218,4 kN | 49100 lbf |
Speed | 974 km/h | 526 kts 605 mph |
Mmo (max. Mach) | Mach 0.9 | |
Service Ceiling | 13.106 m | 43.000 ft |
Range | 5.760 (11.297) km | 3.110 (6.100) NM 3.579 (7.020) mi. |
Empty Weight | 105.687 kg | 233.000 lbs |
max. Takeoff Weight | 231.332 kg | 510.000 lbs |
max. Landing Weight | 166.922 kg | 368.000 lbs |
Wing Span | 47,34 (50,09) m | 155 ft 4 in (164 ft 4 in) |
Wing Area | 320,0 (329,0) m² | 3444 (3541) ft² |
Length | 54,17 (50,05) m | 177 ft 9 in (164 ft 2 in) |
Height | 16,87 m | 55 ft 4 in |
First Flight | 17.11.1970 | |
Production Status | out of production | |
Production Range | 1971-1983 | |
Total Production | 250 |
ICAO Code | L101 | |
IATA Code | L10 L11 L15 L1F | |
FAA TCDS | A23WE | |
Data for (Version) | Lockheed L-1011-1 (L-1011-500) | |
Variants | L-1011-1 (L-1011-385-1), L-1011-100 (L-1011-385-1-14 /-15), L-1011-200 (L-1011-385-1-15), L-1011-500 (L-1011-385-3) |
[Photo-ID: 11970] © Karsten Palt 2001-07-27 | |
Lockheed L-1011-K1 Royal Air Force Reg.: ZD949 c/n: 1159 | |
Royal International Air Tattoo 2001 [Royal Air Force Station Cottesmore (EGXJ)] |