Ver video

ULM

SIDE BY SIDE

OVERVIEW

Experience. Design.

The objective of this project was to develop a two seat helicopter that fitted the ULM category, based on the platform of the Cicaré 7B and 7T. This model will also be sold as a kit.

We prioritized low fuel consumption, operation cost, and the lowest empty weight to achieve higher payload. To accomplish this we incorporated latest technology materials.

All the experience of Augusto Cicaré and its technical, engineering and design team are present in this new product that manifest the innovation, reliability, quality, maneuverability and efficiency that is well known within Cicaré products.

Cicaré 8

FEATURES

TECHNICAL SPECS

Technical Specs Section Technical Specs Section

Engine

EPA R917 Ti

135 HP

Weight

Empty: 280 Kg. (620lb)

MTOW: 480 Kg. (1060lb)

Performance

VNE: 194 Km/h

Cruise speed: 150 km/h

Climb rate: 7 m/s - 1400 ft/min

Service Ceiling: 4500 m.

Fuel

Type: 95 octane

Endurance: 2,5 hrs