Statements (58)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:avionics |
modern avionics
|
| gptkbp:cockpit |
glass cockpit
|
| gptkbp:crew |
2
|
| gptkbp:cruise_speed |
540 mph
|
| gptkbp:design |
wide-body airliner
|
| gptkbp:engine_type |
gptkb:Rolls-Royce_RB211
|
| gptkbp:first_delivery |
1972-04-01
|
| gptkbp:first_flight |
2006-12-01
1970-11-16 |
| gptkbp:fuel_capacity |
30,000 US gallons
|
| gptkbp:fuselage_material |
monocoque
|
| gptkbp:height |
16.8 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lockheed L-1011-1
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
55.5 m
|
| gptkbp:manufacturer |
gptkb:Lockheed_Corporation
|
| gptkbp:max_speed |
0.84 Mach
|
| gptkbp:max_takeoff_weight |
250,000 lb
|
| gptkbp:notable_features |
advanced aerodynamics
fuel efficiency improved aerodynamics improved passenger experience state-of-the-art technology high reliability high safety standards low noise levels reduced operational costs quiet operation advanced navigation systems increased payload capacity high passenger comfort highly efficient engines advanced engine technology enhanced safety features high altitude performance three-engine design advanced wing design advanced flight control systems long range capabilities state-of-the-art cabin design high cruising altitude twin-aisle configuration |
| gptkbp:number_built |
250
|
| gptkbp:operational_range |
4,000 nautical miles
|
| gptkbp:passenger_capacity |
256
|
| gptkbp:primary_user |
gptkb:Delta_Air_Lines
gptkb:British_Airways gptkb:TWA |
| gptkbp:range |
4,000 mi
|
| gptkbp:retired |
gptkb:2006
|
| gptkbp:service_entry |
gptkb:1972
|
| gptkbp:successor |
gptkb:Lockheed_L-1011-500
|
| gptkbp:wing_area |
3,000 ft²
|
| gptkbp:wing_configuration |
low-wing
|
| gptkbp:wingspan |
47.6 m
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_RB211
|
| gptkbp:bfsLayer |
5
|