En Détail

Item Name

Vue générale

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