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
other · Rule · Final special conditions. · Published 2015-06-25 · Effective 2015-07-27 · 80 FR 36470
Document
Document number
2015-15545
Federal Register citation
80 FR 36470
Type
Rule
Action
Final special conditions.
Category
other
Publication date
2015-06-25
Effective date
2015-07-27
FAA docket
Docket No. FAA-2015-0426
Abstract
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.