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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