The airplane also comprises a horizontal stabiliser and a fin.

The airplane sustained substantial damage to the right horizontal stabilizer.

The airplane had sustained damage to the right horizontal stabilizer.

Accordingly, the present invention is able to resolve the design problem of the horizontal stabilizer caused by a ground effect because the WIG vehicle comprises a canard for stabilizing vertical disturbance instead of a horizontal stabilizer.

This resulted in substantial damage to the right horizontal stabilizer.

The wing assembly has a wing substantially aligned with and parallel to the horizontal stabilizer assembly.

The invention relates to a fairing system for an aircraft horizontal stabiliser of an aircraft and to a process for installing said system.

Solar cells: 11,628 (10,748 on the wing, 880 on the horizontal stabilizer)

Solar cells 11,628 (10,748 on the wing, 880 on the horizontal stabilizer)

The tail defines a structural box having first and second vertical stabilizers that support a horizontal stabilizer.

A horizontal stabiliser is embodied in the form of a rectangle and provided with pitch controls.

The invention also concerns a shell, in particular a fuselage shell, a wing shell, a horizontal stabilizer shell or a vertical stabilizer shell, manufactured in accordance with the inventive method.

A second roll bar is then arranged inboard of the horizontal roll bar, in a linear array along the length of the vehicle, and at an inclined angle relative to the plane of the floor pan.

This is most likely the horizontal stabilizer area in the back of the plane.

The left side of the horizontal stabilizer was broken outboard of the fairing.