It had fixed landing gear, with each mainwheel on a cranked axle assisted by a trailing drag strut, both hinged on the central fuselage underside.
12.
It was an amphibian with retractable wheels on cranked axles with rearward drag struts hinged from the fuselage sides and with near-vertical shock absorber legs.
13.
The JG . 10 had fixed, conventional landing gear, its mainwheels on bent axles with rearward drag struts, all hinged to the central fuselage underside.
14.
Each wheel was hinged on a V-strut from the fuselage side and a narrow V drag strut from the aft spar to the stub axle ends.
15.
Each mainwheel was at the end of a vertical oleo strut mounted on the forward wing spar, together with a rearward drag strut to the lower fuselage longeron.
16.
The mainwheels, equipped with brakes, were independently mounted on bent axles hinged from the central fuselage and restrained by drag struts from the forward lower fuselage frames.
17.
Its tailskid landing gear was fixed, with each mainwheel on its own bent axle from the central fuselage underside and with drag struts back to the lower fuselage frames.
18.
The Potez 37 had fixed, conventional landing gear, with mainwheels, equipped with brakes, placed apart at the ends of half-axles and drag struts hinged to the fuselage.
19.
The Couzinet 101 had similar gear, each wheel with a near-vertical oleo strut to the forward spar in the inner wing and a cranked axle and drag strut from the lower fuselage.
20.
The U 8 had fixed, conventional landing gear of the single axle type which was more refined than that of the U5, with a longer oleo strut to mid-fuselage and rearward drag struts.
