Lockheed L-1011 TriStar
Photo ©: Mike Vallentin
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.
| Crew | 3 | |
| Passengers | 256-400 (246-315) | |
| Propulsion | 3 Turbofan Engines | |
| Engine Model | Rolls-Royce RB.211-22C-02 (RB.211-524B4-02) | |
| Engine Power (each) | 182,5 (218,5) kN | 41030 (49120) 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 | 155,3 (164,3) ft |
| Wing Area | 320,0 (329,0) m² | 3444 (3541) ft² |
| Length | 54,17 (50,05) m | 177,7 (164,2) ft |
| Height | 16,87 m | 55,3 ft |
| First Flight | 17.11.1970 | |
| Production Status | out of production | |
| Production Range | 1971-1983 | |
| Total Production | 250 | |
| 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) | |
Remarks
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.
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| Lockheed Martin Corp. |
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