McDonell Douglass DC-10-30F FedEx
Credits: GalacticaAsia
The DC-10 was designed and built in Long Beach, California. After going into production in January 1968, 386 commercial units were delivered, along with 60 KC-10 tanker/cargo models. The plane was billed to succeed the Douglas DC-8 narrowbody airliner in the long-haul market. Altogether, airlines in the United States were looking for a widebody plane to take on transcontinental services. Many of these operators were looking for something not as gargantuan as the Boeing 747. Therefore, the DC-10 would arrive smaller than the 360-seat Queen of the Skies. However, it would still be larger than the narrowbody jets of the time that were arriving with around 180 seats. Importantly, American Airlines put the word out that it was looking for a solution to take on similar operations to the 747, but from airports with shorter runways.
Specifications
General Characteristics
- Predecessor DC-10-30 KLM
- Created On Windows
- Wingspan 168.2ft (51.3m)
- Length 181.7ft (55.4m)
- Height 59.0ft (18.0m)
- Empty Weight N/A
- Loaded Weight 144,872lbs (65,713kg)
Performance
- Power/Weight Ratio 1.396
- Horse Power/Weight Ratio 0.496
- Wing Loading 30.8lbs/ft2 (150.5kg/m2)
- Wing Area 4,700.5ft2 (436.7m2)
- Drag Points 16004
Parts
- Number of Parts 624
- Control Surfaces 9
- Performance Cost 5,262