Hawker Siddeley HS 121 Trident
GPTKB entity
Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:crew |
3
|
| gptkbp:developedBy |
gptkb:de_Havilland_DH.121
|
| gptkbp:engine |
gptkb:Rolls-Royce_Spey
|
| gptkbp:engineType |
turbojet
|
| gptkbp:firstFlight |
1962-01-09
|
| gptkbp:fuselageConfiguration |
narrow-body
|
| gptkbp:height |
8.23 m
|
| gptkbp:introduced |
1964
|
| gptkbp:length |
35.97 m
|
| gptkbp:manufacturer |
gptkb:Hawker_Siddeley
|
| gptkbp:maximumSpeed |
965 km/h
|
| gptkbp:maxTakeoffWeight |
64,410 kg
|
| gptkbp:notableFor |
first airliner with automatic landing capability
|
| gptkbp:numberBuilt |
117
|
| gptkbp:numberOfEngines |
3
|
| gptkbp:primaryUser |
gptkb:British_European_Airways
gptkb:China_United_Airlines |
| gptkbp:range |
3,700 km
|
| gptkbp:retired |
1995
|
| gptkbp:seatingCapacity |
101
180 |
| gptkbp:status |
retired
|
| gptkbp:successor |
none
|
| gptkbp:tailConfiguration |
T-tail
|
| gptkbp:wingspan |
30.58 m
|
| gptkbp:bfsParent |
gptkb:Hawker_Siddeley
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
Hawker Siddeley HS 121 Trident
|