Douglas DC-9-10
Douglas/McDonnell Douglas

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
Capacitycompared to Boeing 757-300
Passenger Capacity
31% of 757-300 maximum capacity
Crew
Dimensions
Length
Wingspan
Height
Wing Area
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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