Airframer
ProgramsHumbert Tetras

Aircraft program

Humbert Tetras

In production
Logbook Follow this page and keep your own private notes on it — log in to start

Two-seater, high wing, single piston ultralight. Includes the variants Tetras B, CS, CSL, CSR or CTS.

Humbert Tetras
Lift type
Fixed wing
Assembly
Factory-built
Control
Piloted
Engine type
Piston
Application
Ultralight
Final assembly

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
Aluminium
Wing
Fabric-covered
Landing gear
Fixed tricycle
Ice protection
None
Pressurisation
Unpressurised
Systems & avionics
Flight controls
Mechanical
Autopilot
None
Avionics architecture
Analogue
Configuration & certification
Wing position
High
Planform
Straight
Tail
Conventional
continued
Certification
Part 23
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.

A deeper insight into the Humbert Tetras

Supplier geography and market analysis for this program — shown free on sponsored programs, or with an Analytics subscription.

See Analytics rates
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

VariantLaunch / first flightProduction endNotes
Humbert Tetras1992 / 1992Two-seat ultralight aircraft with high, trapezoidal wing.

Airframer

Humbert Aviation

Other aircraft programs

Humbert Moto du Ciel

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

Spotted something wrong or out of date on this page? Tell us

Corrections go straight to the editorial team that maintains this directory.