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DC-9-51
DC-9-51 SPECIFICATIONS
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| Number of aircraft |
8 |
| Seating capacity |
122 |
| Length (m) |
40,7 |
| Wing span (m) |
28,4 |
| Cruising speed (km/h) |
925 |
| Max.cruising altitude (m) |
10 670 |
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DC-9-51 DETAILED SPECIFICATIONS
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| Max. Take-Off Weight (kg) |
55 450 |
| Max Zero-Fuel Weight (kg) |
44 700 |
| Max. Payload (kg) |
13 100 |
| Max. Fuel Capacity (kg) |
15 300 |
Engines JT8D-17A
| Max. Static Thrust (kN) |
2x71,2 |
| Fuel Consumption (kg/h) |
2 950 |
| Take-Off Speed (km/h) |
295 |
| Landing Speed (km/h) |
250 |
Dimensions
| Length (m) |
40,7 |
| Height (m) |
8,6 |
| Wing span (m) |
28,4 |
Performance
| Runway Requirement: Take-Off (m) |
2 510 |
| Runway Requirement: Landing (m) |
1 490 |
| Max. Cruising Speed (km/h) |
925 |
| Range (km) |
1 965 |
| Max. Cruising Altitude (m) |
10 670 |
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