Special Conditions: Airbus Model A380-800 Airplane; Dynamic Braking, \nInteraction of Systems And Structures, Limit Pilot Forces, Side Stick \nControllers, Dive Speed Definition, Electronic Flight Control \nSystem-Lateral-Directional Stability, Longitudinal Stability, And Low Energy \nAwareness, Electronic Flight Control System-Control Surface Awareness, \nElectronic Flight Control System-Flight Characteristics Compliance Via the \nHandling Qualities Rating Method, Flight Envelope Protection-General Limiting \nRequirements, Flight Envelope Protection-Normal Load Factor (G) Limiting, \nFlight Envelope Protection-High Speed Limiting, Flight Envelope \nProtection-Pitch And Roll Limiting, Flight Envelope Protection-High Incidence \nProtection and Alpha-Floor Systems, High Intensity Radiated Fields (HIRF) \nProtection, and Operation Without Normal Electrical Power

These Special Conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These design features include side stick controllers, a body landing gear in addition to conventional wing and nose landing gears, electronic flight control systems, and flight envelope protection. These Special Conditions also pertain to the effects of such novel or unusual design features, such as their effects on the structural performance of the airplane. Finally, the Special Conditions pertain to the effects of certain conditions on these novel or unusual design features, such as the effects of high intensity radiated fields (HIRF) or of operation without normal electrical power. Additional Special Conditions will be issued for other novel or unusual design features of the Airbus A380- 800 airplanes. A list is provided in the section of this document entitled "Discussion of Novel or Unusual Design Features.''