Overview
The de Havilland Comet 4 was a later and improved version of the world’s first commercial jet airliner. Developed after structural redesigns, it reentered service in the late 1950s. The aircraft marked a return to jet operations for British airlines.
Specifications
Units
- Engine
- 4 × Rolls-Royce Avon Mk 524 turbojets
- Engine type
- Jet
- Thrust
- 4 × 10,500 lbf · 47 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 81 economy · 81 business · 56 first
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 111 ft 7 in · 34.00 m
- Tail height
- 29 ft 6 in · 8.99 m
- Fuselage diameter
- —
- Wing span
- 114 ft 10 in · 35.00 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 162,000 lb · 73,500 kg
- Max landing weight
- —
- Max payload
- 24,100 lb · 10,900 kg
- Fuel capacity
- 10,450 gal · 39,500 L · 31,600 kg (Jet A)
- Max cruise speed
- 486 kt · 559 mph · 900 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 2,802 nm · 3,220 mi · 5,190 km
- Fuel burn
- 0.31 nm/gal · 0.15 km/L
- Ceiling
- 42,000 ft · 12,800 m
- Rate of climb
- —
- Takeoff distance
- 7,500 ft · 2,290 m
- Landing distance
- —
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