Tomark Skyper GT9 - program supplier guide | Airframer

Tomark Skyper GT9

In production

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Overview Supply chain (8) Downloads

Two seater sport aircraft.

Lift type

Fixed wing

Assembly

Factory-built

Control

Piloted

Engine type

Piston

Application

Sport, Touring, Trainer

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

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 Tomark Skyper GT9

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The industry ledger — an Analytics feature — holds every dated event on this program: contracts, certifications, first flights and appointments, each linked to its source. See a worked example →

Type variants

Variant	Launch / first flight	Production end	Notes
Tomark Skyper GT9	2014 / 2015		Two-seat side by side ultralight aircraft intended to meet Czech UL-21 and ELSA, Germany UL and US LSA requirements.

Airframer

Tomark s r.o.

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