Indonesian Aerospace NC-212 Specifications
| C-212-400 Aviocar | |
Dimensions | |
|---|---|
| Length (m) | 16.2 |
| Wingspan (m) | 20.3 |
| Height (m) | 6.6 |
| Wing area (m2) | 41.0 |
Weight | |
| Maximum take-off weight (kg) | 8 100 |
| Maximum landing weight (kg) | 8 100 |
| Maximum zero fuel weight (kg) | 7 500 |
| Maximum payload (kg) | 2 950 |
| Standard fuel capacity (litres) | 2 000 |
Performance | |
| Range with max payload (km) | 740 |
| Cruise speed (km/h) | 300 |
| Maximum speed (km/h) | 360 |
| Maximum operating altitude (m) | 7 900 |
| Take-off field length (m) | 820 |
| Landing field length (m) | 860 |
| Engines | Honeywell TPE331-12JR, 2 x 925 hp |
Cabin Data | |
| Passengers (1-class) | 24 |
| Cabin width (m) | 2.1 |
Indonesian Aerospace NC-212 Airplane
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