Airframer
Quintus Technologies Quintus Technologies
ProgramsRoland Z-120 Relax

Aircraft program

Roland Z-120 Relax

In production
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Single-seat ultralight aircraft with removable wings, sweptback fin and low, constand chord tailplane.

Lift type
Fixed wing
Construction
Kit-built
Control
Piloted
Engine type
Piston, Rotary
Application
Ultralight
Final assembly
Mendig ·

Design & construction

Primary structure
Composite
Wing
Composite
Landing gear
Fixed tricycle
Ice protection
None
Pressurisation
Unpressurised
Flight controls
Mechanical
Autopilot
None
Avionics architecture
Analogue
Environmental control
None-unpressurised
Wing position
Low
Planform
Straight
Tail
Conventional
Certification
Experimental-LSA
Minimum crew
1
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

VariantLaunch / first flightProduction endNotes
Roland Z-120 Relax2015 / 2105Ultralight aircraft, complies with German 120 kg class rules.

Airframer

Roland Aircraft

Other aircraft programs: Roland S-STOL · Roland Z-602 ·

Find other programs with these properties in the aircraft programs directory.

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