Airframer
Programs › Cicaré CH-7B Spirit

Aircraft program

Cicaré CH-7B Spirit

In production
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The single seat CH-7B Spirit, CH-7BT, similar to CH-7B, but with Rotax 914 engine and CH-7T Tandem Spirit- two seater version. First flight was proof-of-concept CH-2002 in Sept 2001, whilst the CH-12 two-seater type proof-of-concept first flew Sept 2001 with a second prototype flying by 2013. The CH-8 single-seat prototype first flew in 2010.

This is a sports helicopter with steel and aluminium chassis structure.

Cicaré CH-7B Spirit
Lift type
Rotary wing
Assembly
Factory-built, Kit-built
Control
Piloted
Engine type
Piston
Application
Sport, Ultralight

Design & construction

The aircraft as engineered: what it is built from, the systems it flies with, and its configuration — each box a theme.

Airframe & structure
Landing gear
Skids
Ice protection
None
Pressurisation
Unpressurised
Systems & avionics
Flight controls
Mechanical
Autopilot
None
Avionics architecture
Analogue
Configuration & certification
Rotor configuration
Single main + tail
Certification
Part 27
Minimum crew
1

Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.

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Type variants

VariantLaunch / first flightProduction endNotes
Cicaré CH-7B Spirit2010 / 2010Single-seat ultralight helicopter.
Cicaré CH-7T Tandem Spirit2012 / 2010Two-seat ultralight helicopter.

Airframer

Cicaré S.A.

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