Overview
The Lockheed L-1011 TriStar 500 was a shorter-range and shorter-fuselage variant of the TriStar widebody. Designed for medium and long-haul routes, it combined advanced systems with a trijet configuration. The aircraft entered service in the late 1970s.
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Specifications
Units
- Engine
- 3 × Rolls-Royce RB.211-524B
- Engine type
- Turbofan
- Thrust
- 3 × 50,000 lbf · 222 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 246 economy · 253 business · 234 first
- Crew
- —
- Cabin width
- 19 ft 0 in · 5.80 m
- Cabin height
- 7 ft 10 in · 2.40 m
- Cabin length
- 135 ft 10 in · 41.40 m
- Exterior length
- 164 ft 2 in · 50.05 m
- Tail height
- 55 ft 1 in · 16.80 m
- Fuselage diameter
- 19 ft 8 in · 6.00 m
- Wing span
- 164 ft 4 in · 50.10 m
- Baggage volume
- 14,832 ft³ · 420.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 510,000 lb · 231,500 kg
- Max landing weight
- —
- Max payload
- 92,500 lb · 42,000 kg
- Fuel capacity
- 31,650 gal · 119,800 L · 95,800 kg (Jet A)
- Max cruise speed
- 525 kt · 604 mph · 972 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 5,349 nm · 6,160 mi · 9,910 km
- Fuel burn
- 0.12 nm/gal · 0.06 km/L
- Ceiling
- 43,000 ft · 13,100 m
- Rate of climb
- 2,820 ft/min · 14 m/s
- Takeoff distance
- 7,950 ft · 2,430 m
- Landing distance
- 5,700 ft · 1,730 m
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