Statements (55)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:aircraft
|
gptkbp:bfsLayer |
5
|
gptkbp:bfsParent |
gptkb:No._32_(The_Royal)_Squadron_RAF
|
gptkbp:crew |
2 pilots
|
gptkbp:design |
Lockheed engineers
|
gptkbp:engine_type |
Rolls-Royce R B211
|
gptkbp:first_flight |
1970-11-16
|
https://www.w3.org/2000/01/rdf-schema#label |
Lockheed Tri Star
|
gptkbp:is_used_by |
gptkb:Pan_Am
gptkb:Air_Canada gptkb:Delta_Air_Lines gptkb:British_Airways gptkb:TWA |
gptkbp:length |
55.5 m
|
gptkbp:manufacturer |
gptkb:Lockheed_Corporation
|
gptkbp:max_takeoff_weight |
250,000 lb
|
gptkbp:notable_features |
gptkb:military_base
advanced aerodynamics low noise levels high fuel efficiency quiet operation advanced navigation systems improved safety features fly-by-wire controls high passenger comfort spacious cabin large cargo door high altitude performance high bypass turbofan engines three-engine design wide-body fuselage efficient fuel consumption long-range capabilities modern cockpit design versatile operational capabilities wing-mounted engines reduced drag design comfortable seating arrangement dual aisle configuration tail-mounted stabilizer cargo and passenger configurations |
gptkbp:number_built |
250
|
gptkbp:origin |
gptkb:United_States
|
gptkbp:range |
5,000 miles
|
gptkbp:retired |
gptkb:2008
|
gptkbp:role |
wide-body airliner
|
gptkbp:seating_capacity |
250
|
gptkbp:services |
gptkb:1972
|
gptkbp:speed |
0.84 Mach
|
gptkbp:successor |
gptkb:Lockheed_L-1011_Tri_Star
|
gptkbp:variant |
gptkb:L-1011-1
gptkb:L-1011-100 gptkb:L-1011-500 gptkb:L-1011-200 |
gptkbp:wingspan |
47.6 m
|