Douglas DC-8-61

ICAO aircraft code DC86
Manufacturer Douglas Aircraft Co.
Country United States

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Douglas DC-8-61 specifications

General

ICAO aircraft code
DC86
Manufacturer
Douglas Aircraft Co.
Manufactured
1966 - 1972
Country
United States

Aircraft performance

Engine:
4x P&W JT3D-3B
Turbofan
Power:
18,000 pound-force
Max Cruise Speed:
483 Kts
895 Km/h
Approach Speed (Vref):
140 Kts
Travel range:
3,200 Nm
5,926 Kilometers
Service Ceiling:
42,000 feet
Rate of Climb:
2000 feet / minute
10.16meter / second
Take Off Distance:
3000 meter - 9,842.40 feet
Landing Distance:
2000 meter - 6,561.60 feet

Weight & dimensions

Max Take Off Weight:
147,400 Kg
324,958 lbs
Max Landing Weight:
108,000 Kg
238,097 lbs
Max Payload:
27,400 Kg
60,406 lbs
Fuel Tank Capacity:
23,393 gallon
88,552 liter
Baggage Volume:
45.7 m3 / 1,614 ft3

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

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