McDonnell Douglas DC-9-30 specs
| Manufacturer: | McDonnell Douglas |
| Country: |  United States of America |
| ICAO Type designator: | DC93 |
| First flight: | 1 August 1966 |
| Production ended: | 1982 |
| Production total: | 662 |
| Series: | C-9: Aeromedical evacuation aircraft based on the DC-9-32CF
DC-9-30: -10 with 14 ft 9 in (4.50 m) fuselage stretch, improved wing and full-span leading edge slats DC-9-31: Passenger version of -30 series DC-9-32: All Freight (AF), Convertible Freight (CF) versions DC-9-33: All Freight (AF), Convertible Freight (CF) and Rapid Change (RC) versions |
| Propulsion: | 2 jet engines |
| Maximum number of passengers: | 127 |
| Maximum take-off mass: | 54885 kg |
| ICAO Mass group: | 4 |
| Design Service Objective: | 40000 flights |
| Design Service Objective: | 30000 flight hours |
| Design Service Objective: | 20 years |
McDonnell Douglas DC-9-30 file photo (photo: Aviation Safety Network archives)
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