Special Conditions: Dassault Aviation Model Falcon 7X Airplane; Side Stick \nControllers, Electronic Flight Control System: Lateral- Directional and \nLongitudinal Stability, Low Energy Awareness, Flight Control Surface Position \nAwareness, and Flight Characteristics Compliance Via the Handling Qualities \nRating Method; Flight Envelope Protection: General Limiting Requirements, High \nIncidence Protection Function, Normal Load Factor (g) Limiting, and Pitch, \nRoll, and High Speed Limiting Functions
Special conditions are rules the FAA writes for one design when the standard certification rules do not cover something new about it. These were published April 11, 2007 for Dassault Aviation. System: flight controls.
What it applies to
- Applicant
- Dassault Aviation
- Makes
- Dassault
- Models
- —
- Published
- April 11, 2007
- Effective
- April 3, 2007
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
These special conditions are issued for the Dassault Aviation Model Falcon 7X 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, electronic flight control systems, and flight envelope protections. These special conditions pertain to control and handling qualities of the airplane and protection limits within the normal flight envelope. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.
