Overview
The Douglas DC-8-53 was part of the Series 50 generation introduced in the early 1960s. Designed to improve fuel efficiency and extend range over earlier variants, it helped airlines expand long-haul networks. The aircraft became a key jetliner of the intercontinental era.
Live Fleet Activity (DC85)
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Specifications
Units
- Engine
- 4 × Pratt and Whitney JT3D-3B
- Engine type
- Turbofan
- Thrust
- 4 × 18,000 lbf · 80 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 189
- Crew
- —
- Cabin width
- 11 ft 6 in · 3.50 m
- Cabin height
- 7 ft 3 in · 2.21 m
- Cabin length
- 127 ft 11 in · 39.00 m
- Exterior length
- 150 ft 7 in · 45.90 m
- Tail height
- 43 ft 4 in · 13.21 m
- Fuselage diameter
- 12 ft 3 in · 3.74 m
- Wing span
- 142 ft 5 in · 43.40 m
- Baggage volume
- 1,391 ft³ · 39.4 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 325,000 lb · 147,500 kg
- Max landing weight
- 240,000 lb · 109,000 kg
- Max payload
- 101,000 lb · 45,800 kg
- Fuel capacity
- 23,450 gal · 88,800 L · 71,100 kg (Jet A)
- Max cruise speed
- 483 kt · 556 mph · 895 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 137 kt · 158 mph · 254 km/h
- Range
- 4,960 nm · 5,710 mi · 9,190 km
- Fuel burn
- —
- Ceiling
- 36,000 ft · 11,000 m
- Rate of climb
- 1,300 ft/min · 7 m/s
- Takeoff distance
- 9,850 ft · 3,000 m
- Landing distance
- 6,550 ft · 2,000 m
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