Overview
The Xian MA60 is a twin-turboprop regional airliner developed in China. Introduced in the early 2000s, it was designed to serve short-haul markets. The aircraft is based on earlier Chinese turboprop designs.
Live Fleet Activity (MA60)
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Specifications
Units
- Engine
- 2 × Pratt & Whitney Canada PW127J
- Engine type
- Turboprop
- Power
- 2 × 2,750 shp · 2,051 kW
- Avionics
- Rockwell Collins Pro-Line 21
- Wing tips
- No winglets
- Seats
- 64
- Crew
- —
- Cabin width
- 8 ft 10 in · 2.70 m
- Cabin height
- 6 ft 3 in · 1.90 m
- Cabin length
- 35 ft 5 in · 10.80 m
- Exterior length
- 81 ft 0 in · 24.70 m
- Tail height
- 29 ft 1 in · 8.86 m
- Fuselage diameter
- 9 ft 6 in · 2.90 m
- Wing span
- 95 ft 10 in · 29.20 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 48,100 lb · 21,800 kg
- Max landing weight
- 47,600 lb · 21,600 kg
- Max payload
- 12,100 lb · 5,500 kg
- Fuel capacity
- 1,480 gal · 5,600 L · 4,500 kg (Jet A)
- Max cruise speed
- 278 kt · 320 mph · 515 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 860 nm · 990 mi · 1,590 km
- Fuel burn
- —
- Ceiling
- 25,000 ft · 7,600 m
- Rate of climb
- 1,500 ft/min · 8 m/s
- Takeoff distance
- 5,900 ft · 1,800 m
- Landing distance
- 5,250 ft · 1,600 m
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Live fleet activity details
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