Airframer
ProgramsBelmont Patino

Aircraft program

Belmont Patino

In production
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The fuselage of this metal aircraft has a duralumin cover and duralumin reinforcements. The cabin is fitted with organic glass in a composite frame and the pilot seats are made of composite sandwich. The wing is metal, finished with composite end arches.

The horizontal tail is formed by a stabiliser and a rudder. The stabiliser is a two-beam metal shell with composite end bends. The rudder construction is all metal.

The vertical tail consists of a keel of two-beam construction and metal rudder composed of beam, ribs and cover. The end of the keel and rudder is composed of composite arches.

The aircraft has a double hand control mechanical drawbar for elevator and ailerons. The foot control of the rudder is also dual and is rope. Steel cables are suspended between the inner pedals and the eyes of the rudder control pattern located on the keel.

The aircraft has a solid three wheel landing gear with steerable nose wheel. The main chassis wheels are equipped with hydraulic brakes controlled by the brake lever from the cab.

Belmont Patino
Lift type
Fixed wing
Assembly
Factory-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
Ice protection
None
Pressurisation
Unpressurised
Configuration & certification
Certification
Experimental-LSA
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
Belmont DW 210 RG / 2020Upgraded retractable landing gear variant.
Belmont DW 2002018 / 2018Two-seater lightplane, also known as Patino Classic.

Airframer

Belmont Aero SIA

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

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