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Hawker Siddeley HS-121 Trident specs
 
Manufacturer:Hawker Siddeley Aviation
Country: United Kingdom
First flight:9 January 1962
Production ended: 1975
Production total:117
Series: Hawker Siddeley HS-121 Trident 1C: Production version
Hawker Siddeley HS-121 Trident 1E: Increased seating capacity uprated engines and addition of leading edge slats
Hawker Siddeley HS-121 Trident 2E: Trident 1E version with triplex autoland system
Hawker Siddeley HS-121 Trident 3B: Trident 2E with a 16 ft 5 in (5.00 m) stretch, and an RB.162 booster engine in the tail
Propulsion:3 jet engines
Maximum number of passengers:180
Maximum take-off mass:68040 kg
ICAO Mass group:4

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