Douglas DC-8-70

Douglas/McDonnell Douglas

ICAODC87IATA388
Douglas DC-8-70 aircraft
Douglas/McDonnell DouglasDouglas DC-8-70
Photo: Björn Strey · CC BY-SA 2.0 · Modified

About

The Douglas DC-8-70 series represents a re-engining program conducted in the 1980s to modernize DC-8-60 aircraft with fuel-efficient CFM International CFM56-2 turbofan engines. This conversion program, offered by Cammacorp (later acquired by Pemco), replaced the original Pratt & Whitney JT3D engines with modern high-bypass CFM56 engines producing 97.9 kN (22,000 lbf) thrust each. The re-engining dramatically improved fuel efficiency by approximately 25%, reduced noise levels to meet stricter regulations, and extended the aircraft's operational life. Three variants mirrored the -60 series: DC-8-71 (Series 61 airframe), DC-8-72 (Series 62 airframe), and DC-8-73 (Series 63 airframe). The program converted 110 aircraft between 1981 and 1988. While passenger range decreased slightly to 8,949 km (4,830 NM) due to the heavier engines, the operational economics made DC-8-70s competitive well into the 1990s. Many DC-8-70s continue operating as freighters today, benefiting from modern engines and proven reliability.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

162,389kg
0
100k
162k

MTOW (Maximum Takeoff Weight)

161,028kg
0
100k
161k

MLW (Maximum Landing Weight)

117,029kg
0
50k
100k
117k

MZFW (Maximum Zero Fuel Weight)

104,328kg
0
50k
104k

Empty Weight

75,388kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

259passengers
0
100
200
295

88% of 757-300 maximum capacity

Crew

Total
9
Cockpit
3
Cabin
6

Dimensions

Length

57.1m

Wingspan

45.2m

Height

12.9m

Wing Area

271.9m²

Catalog Price

Base List Price

$15M USD

1985 catalog price

Note: Actual prices vary based on configuration, options, and negotiations. This represents the manufacturer's base catalog price.

Engine Specifications

Engine Count

4×

Engine Model

CFM International CFM56-2C5

Thrust per Engine

97.9 kN(22009 lbf)

Fuel & Cargo

Fuel Capacity

93,270 L

Cargo Volume

158 m³

Production & History

Total Produced

110

Production Status

Out of production

Manufacturing Period

1981–1988

First Flight

August 15, 1981

Entered Service

April 25, 1982

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