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Programs › SE Aviation MCR Evolution

Aircraft program

SE Aviation MCR Evolution

In production
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Kitbuilt low-wing single-piston light aircraft. Formerly known as Dyn'Aero MCR 4S. Includes MCR 4S Evolution, MCR Pick Up Evolution, MCR ULC Evolution, MCR M Evolution, MCR R100, and an in development UAV variant: Driade.

Lift type
Fixed wing
Assembly
Factory-built, Kit-built
Control
Piloted, Autonomous
Engine type
Piston
Application
Agricultural, Surveillance, Touring, Ultralight, Utility

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
Primary structure
Composite
Wing
Composite
Landing gear
Fixed tricycle
Ice protection
None
Pressurisation
Unpressurised
Systems & avionics
Flight controls
Mechanical
Autopilot
2-axis
Avionics architecture
Standalone glass
Configuration & certification
Wing position
Low
Planform
Straight
Tail
Conventional
continued
Certification
Part 23
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
Dyn'Aero MCR 4S / 20002012Baseline variant, derived from Dyn'Aéro MCR01.
SE Aviation MCR Pick Up Evolution / Ultralight variant of MCR 4S Evolution. Includes more efficient ultralight variant: MCR ULC Evolution.
SE Aviation MCR 4S Evolution / SE Aviation's first development of the MCR program.
SE Aviation MCR M Evolution / Derived from MCR ULC Evolution but not an ultralight, available with tricyle landing gear version or taildraggers.
SE Aviation MCR R100 / Glider variant of MCR ULC Evolution.
SE Aviation Driade2025 / MALE UAS variant with 820 kg MTOW, configured as Driade Reconnaissance (ISR variant), or Driade Intervention (spraying variant with drone swarm ability).

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