Douglas DC-9-10

Douglas/McDonnell Douglas

ICAODC91IATAD91
Douglas DC-9-10 aircraft
Douglas/McDonnell DouglasDouglas DC-9-10
Photo: Hugh Llewelyn from Keynsham, UK · CC BY-SA 2.0 · Modified

About

The Douglas DC-9-10 represents the original production version of the DC-9 family, designed for short-haul domestic routes and optimized for operations from smaller airports. Introduced in 1965, it featured a compact 31.82-meter fuselage seating 80-90 passengers in typical configuration, powered by two Pratt & Whitney JT8D-5 or JT8D-7 turbofans producing 62.3 kN (14,000 lbf) thrust each. Its distinctive rear-mounted engines and T-tail design provided excellent low-speed handling and quiet cabin environment. The DC-9-10's short field performance and economical operations made it ideal for serving secondary cities. Launch customer Delta Air Lines began service in December 1965. The variant proved popular with regional and domestic carriers including Trans World Airlines and Hawaiian Airlines. With a range of 2,335 km (1,265 NM), it excelled on routes like Los Angeles-San Francisco and New York-Boston. A total of 137 DC-9-10s were built before production shifted to larger variants. Many served into the 1990s before retirement.

Weightscompared to Boeing 757-300

MRW (Maximum Ramp Weight)

41,504kg
0
50k
100k
124k

MTOW (Maximum Takeoff Weight)

41,141kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

37,058kg
0
50k
102k

MZFW (Maximum Zero Fuel Weight)

33,566kg
0
50k
95k

Empty Weight

22,300kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

90passengers
0
100
200
295

31% of 757-300 maximum capacity

Crew

Total
4
Cockpit
2
Cabin
2

Dimensions

Length

31.8m

Wingspan

27.3m

Height

8.4m

Wing Area

86.8m²

Catalog Price

Base List Price

$3.5M USD

1966 catalog price

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

Engine Specifications

Engine Count

2×

Engine Model

Pratt & Whitney JT8D-5/7

Thrust per Engine

62.3 kN(14006 lbf)

Fuel & Cargo

Fuel Capacity

13,249 L

Cargo Volume

18.7 m³

Production & History

Total Produced

137

Production Status

Out of production

Manufacturing Period

1965–1968

First Flight

February 25, 1965

Entered Service

December 8, 1965

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