Overview
The Douglas DC-8 was a four-engine jet airliner developed to compete in the early jet transport market. Entering service in 1959, it became a cornerstone of long-haul airline operations. The aircraft evolved through multiple series with increased range and capacity.
Specifications
Units
- Engine
- —
- Engine type
- -
- Thrust
- 19,000 lbf · 85 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 259 economy · 180 business
- Crew
- —
- Cabin width
- 10 ft 7 in · 3.22 m
- Cabin height
- 6 ft 11 in · 2.10 m
- Cabin length
- 145 ft 0 in · 44.19 m
- Exterior length
- 187 ft 4 in · 57.10 m
- Tail height
- —
- Fuselage diameter
- 12 ft 2 in · 3.71 m
- Wing span
- 148 ft 5 in · 45.24 m
- Baggage volume
- 2,500 ft³ · 70.8 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 355,000 lb · 161,000 kg
- Max landing weight
- —
- Max payload
- 34,400 lb · 15,600 kg
- Fuel capacity
- 23,750 gal · 89,900 L · 71,900 kg (Jet A)
- Max cruise speed
- 518 kt · 596 mph · 959 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,860 nm · 2,140 mi · 3,440 km
- Fuel burn
- 0.08 nm/gal · 0.04 km/L
- Ceiling
- 35,000 ft · 10,700 m
- Rate of climb
- —
- Takeoff distance
- 10,000 ft · 3,050 m
- Landing distance
- 6,500 ft · 1,980 m
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