Trident 2E
E373621
Trident 2E is a stretched, higher-capacity variant of the Hawker Siddeley Trident airliner designed to improve range and passenger load.
All labels observed (1)
| Label | Occurrences |
|---|---|
| Trident 2E canonical | 1 |
Statements (36)
| Predicate | Object |
|---|---|
| instanceOf |
Hawker Siddeley Trident variant
ⓘ
airliner variant ⓘ narrow-body jet airliner ⓘ |
| aircraftCategory | civil transport aircraft ⓘ |
| aircraftFamily | Hawker Siddeley Trident ⓘ |
| aircraftLayout | trijet ⓘ |
| aircraftRole | short- to medium-haul airliner ⓘ |
| airframeBasis | Hawker Siddeley Trident ⓘ |
| airlineServiceType | scheduled passenger services ⓘ |
| cockpitCrew | 3 ⓘ |
| construction | all-metal ⓘ |
| countryOfOrigin | United Kingdom ⓘ |
| crewType | two-pilot plus flight engineer ⓘ |
| designEra | 1960s ⓘ |
| designFeature |
increased fuel capacity
ⓘ
increased passenger capacity ⓘ stretched fuselage ⓘ |
| designGoal |
improved passenger load
ⓘ
improved range ⓘ |
| engineConfiguration | rear-mounted ⓘ |
| engineModel |
Rolls-Royce Spey turbofan
ⓘ
surface form:
Rolls-Royce Spey
|
| engineType | turbofan ⓘ |
| enteredService | unknown ⓘ |
| firstFlight | unknown ⓘ |
| jetAge | second-generation jet airliner ⓘ |
| landingGear | tricycle landing gear ⓘ |
| manufacturer |
Hawker Siddeley
ⓘ
surface form:
Hawker Siddeley Aviation
|
| marketSegment | short- and medium-range routes ⓘ |
| numberOfEngines | 3 ⓘ |
| predecessor | Trident 1C ⓘ |
| pressurisation | cabin pressurised ⓘ |
| pressurisedCabin | yes ⓘ |
| primaryUse | commercial passenger transport ⓘ |
| propulsionPlacement | aft fuselage ⓘ |
| tailConfiguration | T-tail ⓘ |
| wingConfiguration | low-wing ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.