Atec 212 Solo - program supplier guide | Airframer

Atec 212 Solo

In production

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Overview Supply chain (4) Downloads

Low wing single piston composite ultralight. Available as kit or factory assembled.

Lift type

Fixed wing

Assembly

Factory-built, Kit-built

Control

Piloted

Engine type

Piston

Application

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

Primary structure

Composite

Wing

Composite

Landing gear

Retractable 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

Experimental-LSA

Minimum crew

Notable technologies — each tag names a technology on our research record for this aircraft, with its fitting status: Primary, Standard, Option or Planned.

Composite wing (primary structure) Primary Composite fuselage (primary structure) Primary

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

A deeper insight into the Atec 212 Solo

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Type variants

Variant	Launch / first flight	Production end	Notes
Atec 212 Solo	2005 / 2005		Ultralight single-seat cantilever wing aircraft.

Airframer

Atec v.o.s.

Other aircraft programs

Atec 321 Faeta/122 Zephyr

Information on this page is compiled from a variety of published sources; links do not necessarily imply recommendation or confirmation by the airframe manufacturer.