McDonnell Douglas DC-10 specs
| Manufacturer: | McDonnell Douglas |
| Country: |  United States of America |
| ICAO Type designator: | DC10 |
| First flight: | 29 August 1970 |
| Production ended: | 1989 |
| Production total: | 446 |
| Series: | DC-10-10: Initial passenger version
DC-10-10CF: Convertible passenger and cargo transport version of the -10 DC-10-10F: Cargo transport version of the -10 DC-10-30: Long-range model with General Electric CF6-50 turbofan engines DC-10-30CF: Convertible cargo/passenger transport version of the -30 DC-10-30ER: Extended-range version of the -30 DC-10-30F: Cargo transport version of the -30 DC-10-40: Long-range version fitted with Pratt & Whitney JT9D engines DC-10-40F: Cargo transport version of the -40 KC-10A: Aerial refueling tanker aircraft modification of -30CF MD-10: Retrofit cockpit upgrade to the DC-10 |
| Propulsion: | 3 jet engines |
| Maximum number of passengers: | 380 |
| Maximum take-off mass: | 263085 kg |
| ICAO Mass group: | 4 |
| Design Service Objective: | 30000 flights |
| Design Service Objective: | 60000 flight hours |
| Design Service Objective: | 20 years |
McDonnell Douglas DC-10 file photo (photo: Aviation Safety Network archives)
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