McDonnell Douglas DC-8-52

Mid Size Passenger Jets

ICAO aircraft code DC85

Manufacturer McDonnell Douglas

Country United States

New price USD 6.5 million (1961)

The DC-8-52 is one of the versions of the DC-8 narrow-body airliner built by the Douglas Aircraft Company.

Specifications

Full description

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McDonnell Douglas DC-8-52 specifications

General

ICAO aircraft code

DC85

Manufacturer

McDonnell Douglas

Manufactured

1958 - 1972

Country

United States

New purchase price

USD 6.5 million (1961)

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):

149 Kts

Travel range:

5,855 Nm
10,843 Kilometers

Service Ceiling:

35,000 feet

Rate of Climb:

1300 feet / minute
6.60meter / second

Take Off Distance:

3000 meter - 9,842.40 feet

Landing Distance:

2000 meter - 6,561.60 feet

Weight & dimensions

Max Take Off Weight:

142,883 Kg
315,000 lbs

Max Landing Weight:

108,860 Kg
239,993 lbs

Max Payload:

23,587 Kg
52,000 lbs

Fuel Tank Capacity:

23,393 gallon
88,552 liter

Baggage Volume:

39.4 m3 / 1,391 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.

About the McDonnell Douglas DC-8-52

The DC-8-52 is one of the versions of the DC-8 narrow-body airliner built by the Douglas Aircraft Company. It is powered by Pratt and Whitney JT3D-3B engines with a maximum rated thrust of 18,000 lbf each.