MA60 | |
Dimensions | |
Length (m) | 24.7 |
Wingspan (m) | 29.2 |
Height (m) | 8.8 |
Weight | |
Maximum take-off weight (kg) | 21 800 |
Maximum landing weight (kg) | 21 600 |
Operating empty weight (kg) | 13 700 |
Maximum zero fuel weight (kg) | 19 200 |
Maximum payload (kg) | 5 500 |
Max stock of fuel (kg) | 4 030 |
Performance | |
Maximum range (km) | 2 450 |
Range with max payload (km) | 1 600 |
Cruise speed (km/h) | 430 |
Maximum speed (km/h) | 514 |
Maximum operating altitude (m) | 7 600 |
Engines | P&WC PW127J , 2 x 2750 hp |
Cabin Data | |
Cabin length (m) | 10.8 |
Cabin width (m) | 2.7 |
Cabin height (m) | 1.9 |
Aisle width (m) | 0.43 |
Monday, May 9, 2011
Xian MA60 Specifications
The Xian MA60 is a turboprop-powered commercial aircraft made by China's AVIC I (China Aviation Industry Corporation I). It is developed from the popular Russian regional aircraft Antonov An-24. With modern powerplant, equipment and design concept the MA60 is suitable for short and medium-haul commuter services. First MA60s were put into operations in 2004.
Labels:
MA60,
Specifications,
Xian
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