Special Conditions: Bombardier Aerospace Incorporated, Models BD- 500-1A10 and BD-500-1A11 Series Airplanes; Electronic Flight-Control System (EFCS): Pitch-and Roll-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 June 24, 2015 for Bombardier Aerospace, covering the BD-500-1A10, BD-500-1A11. System: flight controls.
What it applies to
- Applicant
- Bombardier Aerospace
- Makes
- Bombardier Aerospace
- Models
- BD-500-1A10, BD-500-1A11
- On this site
- Airbus BD-500 182 registered
- Published
- June 24, 2015
- Effective
- July 26, 2015
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
These special conditions are issued for the Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 series airplanes. These airplanes will have a novel or unusual design feature associated with a fly-by-wire EFCS that limits pitch- and roll-limiting functions to prevent the airplane from attaining certain pitch attitudes and roll angles. This system generates the actual surface commands that provide for stability augmentation and flight control for all three airplane axes (longitudinal, lateral, and directional). The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
