Quick Overview
A project with the objective of production of an ultra-light, multi-purpose helicopter of low production & maintenance cost to meet the demand of organizations, institutes and individuals for such type of aircraft.
Product Description
General Specifiations:
A project with the objective of production of an ultra-light, multi-purpose helicopter of low production & maintenance cost to meet the demand of organizations, institutes and individuals for such type of aircraft.
Estimated Weights:
| Description | Weight (Kg) |
| Max. Take of Weight | 650 kg |
| Max. Payload Weight | 270 kg |
| Empty Weight | 380 kg |
Performance Characteristics:
| Max. airspeed | 186 Km/h |
| Cruising air speed | 160 Km/h |
| Static ceiling for hovering | 1500m |
| Flight Duration (H=500m),5% fuel supply | 3 hrs |
| Practical range, | 320 km |
| Engine Power | 162 hp, 121 kw |
| Engine Working volume | 2500 cm3 |
| Practical Ceiling | 3000m |
Time Between Overhaul (T.B.O):
The overall technical life time (design life) of the helicopter is 2000 flght hours.
The fuel:
Safat -02 uses MOGAS (Motor Gasoline) with octane number 95.
It can be fueled with MOGAS #90 according to the manufacturer.
Packing
