Scoda Aeronautica Super Petrel

In production

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Overview Supply chain (5) Downloads

Kitbuilt/factory finished amphibious aircraft with single piston pusher.

Lift type

Fixed wing

Assembly

Kit-built

Control

Piloted

Engine type

Piston

Application

Amphibious, Ultralight

Final assembly

Sao Paulo (Ipeúna) ·

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

Amphibious-floats

Ice protection

None

Pressurisation

Unpressurised

Systems & avionics

Flight controls

Mechanical

Autopilot

None

Configuration & certification

Wing position

High

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.

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Type variants

Variant	Launch / first flight	Production end	Notes
Scoda Aeronautica Super Petrel	2002 / 2002		Two-seat experimental pusher-engine biplane, current variant Super Petrel LS.

Airframer

Scoda Aeronautica

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