Main landing gear landing-gear system offering
Main landing gear is a landing-gear system offering that supports the aircraft during ground operation and landing. It forms part of an airframe installation, with loads, attachment geometry and actuation requirements defined for the selected aircraft configuration.
Description
The Safran A400M main landing gear is a landing-gear system for a large military transport aircraft, supporting the airframe during taxiing, take-off and landing. It is built by Safran Landing Systems for the Airbus A400M, a four-turboprop airlifter, and it is listed here as a heavy main gear assembly for large fixed-wing aircraft.
Each side of the aircraft has a main gear made of three independent twin-wheel assemblies stowed in the streamlined fuselage sponsons, which gives six wheels per side and twelve on the aircraft. This layout spreads the load over a large footprint, a high-flotation arrangement intended for operation from unprepared and soft surfaces.
The structural components are made of titanium. This choice gives a favourable ratio of strength to weight and a higher resistance to corrosion than many alternative materials, which reduces the maintenance burden in the field. The main gear is listed as 2.3 m in height and 6 m in length.
For an integrator, the relevant points are the fuselage-sponson installation, the independent wheel assemblies and the titanium structure; loads, attachment geometry and actuation requirements follow from the A400M configuration.
The product is used on the A400M for tactical and strategic transport, including operations from rough airstrips.
Specifications
| General | |
|---|---|
| Grade | Aerospace-grade |
| Market | Defense |
| Platform class | Manned aircraft |
| Airframe | Fixed-wing |
| Availability | In production |
| Key specifications | |
| Main material | Titanium structural components.[1] |
Sources
- safran-group.com/products-services/a400m-nose-and-main-landing-gears · checked October 25, 2026
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