Helicopter landing-gear systems and integration

Mecaer Aviation Group supplies landing-gear systems for rotorcraft through design and build-to-print services. Its portfolio includes structural assemblies, retraction equipment and integration with steering, wheels, brakes and aircraft control systems.
Description
The Helicopter landing gear is a helicopter landing-gear system from Mecaer Aviation Group with aerospace-grade grade and dual-use market. Mecaer Aviation Group supplies helicopter landing-gear systems, covering the design and integration of undercarriages for rotary-wing aircraft. As a landing-gear system integrator, it offers both clean-sheet design and build-to-print manufacturing, so an airframe maker can either hand over the requirement or supply its own drawings.
The product range comprises nose landing gears, main landing gears and uplocks. The configuration depends on the aircraft, and the gear can be fixed or retractable. Where retraction is needed, the maker provides hydraulic and electro-mechanical systems, which lets the integrator choose between a hydraulic power source already on the aircraft and an electrically actuated solution, a choice that matters for more-electric rotorcraft and eVTOL concepts.
Beyond the structure, the supplier takes responsibility for integrating the gear with the other systems that act on it: wheels and brakes, steering and the aircraft control systems. This integration scope means one supplier can deliver a complete landing system rather than separate parts, which reduces interface work for the airframe manufacturer.
A test laboratory supports the work. The maker lists drop tests at a sink speed of 13 fps and above, limit, ultimate and fatigue load tests, extension and retraction endurance tests, steering endurance tests, nose gear shimmy dynamic testing and environmental testing covering temperature and EMI/EMC. These tests give the data used to demonstrate that a gear design meets its structural and functional requirements.
Typical applications are main and nose landing-gear assemblies for helicopter programmes and for upgrades of existing ones, and landing systems for larger rotorcraft and vertical-lift aircraft that need retractable gear. Buyers should treat the product as a custom-engineered system, defined together with the supplier for each airframe, rather than as a catalogue part with fixed dimensions.
Specifications
| General | |
|---|---|
| Grade | Aerospace-grade |
| Market | Dual-use |
| Platform class | Heavy UAS (>150 kg), eVTOL, Manned aircraft |
| Airframe | Helicopter[1] |
| Availability | In production |
| Key specifications | |
| Gear type | Rotorcraft main and nose landing-gear systems; configuration dependent.[1] |
| Retraction actuation | Hydraulic and electromechanical retraction options.[1] |
Sources
- mecaer.com/business-units/landing-systems · checked October 19, 2026
A value without a number has no recorded source yet: we are adding it.
Frequently asked questions
What types of retraction systems are available for landing gear?
The company offers both hydraulic and electro-mechanical retraction systems.
What specific load and endurance tests can be performed in the test lab?
The test lab is equipped to perform limit, ultimate, and fatigue load tests, as well as extension/retraction and steering endurance tests.
What is the sink speed capability for drop tests?
The landing gear systems are capable of undergoing drop tests at sink speeds of 13+ fps.
Does the company perform environmental testing on landing gear components?
Yes, the company conducts environmental testing, which includes temperature and EMI/EMC testing.
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