Aquila A211 - program supplier guide | Airframer

Aquila A211

In production

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Low wing single piston composite very light aircraft (VLA). Initial version known as A210. Includes the variants A212 and A414 (in development).

Lift type

Fixed wing

Assembly

Factory-built

Control

Piloted

Engine type

Piston

Application

Ultralight

Final assembly

Schoenhagen ·

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

continued

Certification

Part 23

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.

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Type variants

Variant	Launch / first flight	Notes
Aquila A211	2013 / 2000	Single-engine, two-seat light aircraft, includes variants: A211G, A211GX, and A211G3X.
Aquila A212	2018 / 2018	Turbo charged variant, includes A212GX Turbo variant.
Aquila A414	2022 / 2022	Four-seater variant.

Airframer

Aquila Aviation International GmbH

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