Empennage Sample Clauses

The EMPENNAGE clause defines the requirements and specifications related to the tail assembly of an aircraft, which includes components such as the horizontal and vertical stabilizers, elevators, and rudder. This clause typically outlines the standards for design, materials, installation, and maintenance of the empennage to ensure proper aerodynamic stability and control of the aircraft. By clearly setting these expectations, the clause helps prevent misunderstandings regarding the quality and performance of the empennage, thereby ensuring safety and compliance with regulatory requirements.
Empennage. (a) Vertical stabilizer spars and skin between spars (b) Aft fuselage vertical stabilizer carry-through structure (c) Horizontal stabilizer spars, integral skin and stringers between spars, and pivot fittings
Empennage. (a) Vertical spars and plating between spars (b) Aft fuselage vertical stabilizer carry-through structure (c) Horizontal stabilizer spars, integral plating between spars, and pivot fittings