Overview
The Hawker Siddeley Trident was a three-engine narrow-body jet developed for European short-haul routes. Designed with advanced autopilot systems for its time, it entered service in the 1960s. The aircraft became a key part of British European Airways’ fleet.
Live Fleet Activity (TRID)
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Specifications
Units
- Engine
- 3 × Rolls-Royce RB.163-25 Spey 512
- Engine type
- Turbofan
- Thrust
- 3 × 11,960 lbf · 53 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 180 economy · 115 business
- Crew
- —
- Cabin width
- 11 ft 2 in · 3.40 m
- Cabin height
- 6 ft 7 in · 2.00 m
- Cabin length
- 30 ft 0 in · 9.14 m
- Exterior length
- 131 ft 3 in · 40.00 m
- Tail height
- 28 ft 3 in · 8.60 m
- Fuselage diameter
- 11 ft 10 in · 3.60 m
- Wing span
- 98 ft 1 in · 29.90 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 150,000 lb · 68,000 kg
- Max landing weight
- —
- Max payload
- 32,400 lb · 14,700 kg
- Fuel capacity
- 6,550 gal · 24,700 L · 19,800 kg (Jet A)
- Max cruise speed
- 525 kt · 604 mph · 972 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 2,084 nm · 2,400 mi · 3,860 km
- Fuel burn
- 0.43 nm/gal · 0.21 km/L
- Ceiling
- 35,000 ft · 10,700 m
- Rate of climb
- 3,000 ft/min · 15 m/s
- Takeoff distance
- 2,750 ft · 840 m
- Landing distance
- 2,200 ft · 680 m
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