|
Weight of empty aircraft (KGs)
|
26,000
|
|
Maximum landing weight (KGs)
|
36,740
|
|
Maximum take-off weight (KGs)
|
42,184
|
|
Distance needed for take-off at sea level (metres)
|
1,200
|
|
Distance needed for landing at sea level (metres)
|
1,300
|
|
Payload (KGs)
|
10,800
|
|
Maximum fuel capacity (litres)
|
11,700
|
|
Maximum altitude (feet)
|
31,000
|
|
Fuel burn per hour (litres)
|
2,500
|
|
Cruising speed (kph/MACH)
|
750/0.65
|
|
Fuel endurance (H:Min)
|
4:20
|
|
Range (km)
|
1,600
|
|
Required crew
|
2 pilots
|
|
Minimum required visibility for landing (metres)
|
300
|
|
Engines (number and type)
|
4 ALF-502 R5
|
|
Maximum thrust per engine (KGs)
|
3,161
|
|
Number of containers
|
6
|
|
Available total volume (m³)
|
45
|