Hawker Siddeley Trident

· De Havilland · 3 × Rolls-Royce Spey

Airplanes

Length

34.7472 m

Flat Wing Span

27.1272 m

Height

8.2296 m

Flat Wing Area

126.1623 m²

Max Seating

101

Cruise Speed

937.1112 km/h

Max Ceiling

10668 m

Number of Engines

Aircraft Engine

First Flight

1962-01-09

Entry Into service

1964-04-01

Number Built

117

Maximum Take-Off Weight

48.5344 t (paragliders: kg)

Total Fuel Capacity

17456.99

Maximum Range

2172.615 km

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Hawker Siddeley Trident	48.5344	17456.99	2172.615

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Bristol Type 200	Bristol Siddeley Orpheus	36.8808	27.7368	100	Compare

All data (25 fields)

Name: Hawker Siddeley Trident
Manufacturer: De Havilland
Description: The Hawker Siddeley HS-121 Trident (originally the de Havilland DH.121 and briefly the Airco DH.121) is a British airliner produced by Hawker Siddeley.
First Flight: 1962-01-09
Entry Into service: 1964-04-01
Production End: 1978-01-01
Service End: 1995-01-01
Designer: de Havilland
Type: Narrow-body airliner
Length (m): 34.7472
Height (m): 8.2296
Max Seating: 101
Cruise Speed (km/h): 937.1112
Max Ceiling (m): 10668
Capacity Description: 101 seats
National Origin: United Kingdom
Number Built: 117
Powerplant Description: 3 x Spey RB163-1 Mk505-5
Primary Users: British European Airways, British Airways , CAAC Airlines , Cyprus Airways
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Hawker_Siddeley_Trident
Flat Wing Span (m): 27.1272
Flat Wing Area (m²): 126.1623
Aircraft Engine: Rolls-Royce Spey
Number of Engines: 3