Safat Aircraft Manufacturing and Development Complex
Business Field
Safat Aircraft Manufacturing and Development Complex Provides
- Light Aircraft and drones design
- Production and manufacturing of light aircrafts
- Production and manufacturing of drones
- Providing Engineering solutions through design, applied scientific research and testing.
Projects of The Complex
Safat 01 Light Aircraft
A Leading project of its type in Sudan, with the objective of production of light aircraft exploiting local capabilities of Sudanese staff to melt down the shield and to rise up the competence level of SAFAT employees.
Safat 01 Light Aircraft
A Leading project of its type in Sudan, with the objective of production of light aircraft exploiting local capabilities of Sudanese staff to melt down the shield and to rise up the competence level of SAFAT employees.
Safat 02 Light Helicopter
A project with the objective of production of a light, multi-purpose helicopter of low production & maintenance cost to meet the demand of organizations, institutes and individuals for such type of aircraft.
Safat 03 Light Aircraft
SAFAT 03 is a two-seater primary basic trainer which satisfies all primary training requirements like aerobatic, sail flight, night flight, and instrument flight.
SAFAT03 is a full sheet metal y /air frame with low wing configuration, low fuel consumption and operation cost.
Safat 03 Light Aircraft
SAFAT 03 is a two-seater primary basic trainer which satisfies all primary training requirements like aerobatic, sail flight, night flight, and instrument flight.
SAFAT03 is a full sheet metal y /air frame with low wing configuration, low fuel consumption and operation cost.
Technical Specification
| Characteristics | Description |
|---|---|
| Accommodation | 2 |
| Engine Power | 180 hp (Lycoming) |
| Standard Fuel capacity | 150 L |
| Max. range, No external fuel tanks | 740 km (1140 km with leaned mix) |
| Fuel consumption at maximum range regime | 0.20 L/km (0.13 L/km, leaned mix.) |
| Max. initial rate of clime | 3.2 m/s |
| Service ceiling | 5100 m |
| Takeoff mass with fuel (without under wing loads) | 1080 kg |
| Max. takeoff mass with under wing loads | 1200 kg |
| Overall length | 7.60 m |
| Wing Span | 9.80 m |