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McDonnell Douglas DC-10
Commercial
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Lockheed L-1011 TriStar
Commercial
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|---|---|---|
| Quick facts | ||
| Manufacturer | McDonnell Douglas | Lockheed |
| Type | Wide-body airliners | Wide-body airliners |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1970 | 1970 |
| Status | In service | Retired |
| Units built | 386 | 250 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 55.50 m | 54.17 m |
| Wingspan | 50.40 m | 47.35 m |
| Height | 17.70 m | 16.87 m |
| Wing area | 367.7 m² | 320.0 m² |
| Weights & fuel | ||
| Empty weight | 120,742 kg | 109,000 kg |
| Max. take-off weight | 259,459 kg | 195,045 kg |
| Fuel capacity | 138,165 L | — |
| Performance | ||
| Cruise speed | 908 km/h | 890 km/h |
| Max. Mach | Mach 0.88 | Mach 0.90 |
| Range | 9,600 km | 4,963 km |
| Service ceiling | 12,800 m | 12,800 m |
| Crew & capacity | ||
| Crew | 3 | 3 |
| Seats (typical) | 270 | 256 |
| Seats (max.) | 380 | 400 |
| Powerplant | ||
| Engines | 3 | 3 |
| Engine type | — | — |
| Engine model | General Electric CF6-50C | Rolls-Royce RB211-22B |
| Thrust (each) | 227.0 kN | 187.0 kN |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.