Federal Aviation Administration March 21, 2018 – Federal Register Recent Federal Regulation Documents

Special Conditions: Bombardier Inc. BD-700-2A12 and BD-700-2A13 Airplane; Flight Envelope Protection: Normal Load Factor (g) Limiting
Document Number: 2018-05663
Type: Rule
Date: 2018-03-21
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature will use a fly-by- wire electronic flight control system (EFCS) that will prevent the flight crew from inadvertently or intentionally exceeding the positive or negative airplane limit-load-factor. 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.
Special Conditions: Bombardier Inc. BD-700-2A12 and BD-700-2A13 Airplane; Flight-Envelope Protection: General Limiting Requirements
Document Number: 2018-05662
Type: Rule
Date: 2018-03-21
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is a new control architecture and a full digital-flight-control system that provides comprehensive flight-envelope protections. 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.
Special Conditions: Bombardier Inc., Model BD-700-2A12 and BD-700-2A13 Series Airplanes, Flight Envelope Protection: Pitch and Roll Limiting
Document Number: 2018-05651
Type: Rule
Date: 2018-03-21
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Inc. (Bombardier), Model BD-700-2A12 and BD-700-2A13 series airplanes. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the applicable airworthiness standards for transport-category airplanes. This design feature is the fly-by-wire electronic flight-control system (EFCS) that will limit pitch and roll functions to prevent the airplane from attaining certain pitch attitudes and roll angles. 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.
Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Series Airplanes; Synthetic Vision System on Head-Up Display
Document Number: 2018-05650
Type: Rule
Date: 2018-03-21
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Bombardier Inc. (Bombardier) Model BD-700-2A12 and BD-700-2A13 series airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the applicable airworthiness standards for transport-category airplanes. These airplanes incorporate a novel or unusual design feature associated with a synthetic vision system (SVS) that displays video imagery on the head-up display (HUD). 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.
Proposed Establishment of Class E Airspace; Pago Pago, American Samoa
Document Number: 2018-05585
Type: Proposed Rule
Date: 2018-03-21
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace extending upward from 700 feet above the surface at Pago Pago International Airport, Pago Pago, American Samoa (AS), to accommodate the development of instrument flight rules (IFR) operations under standard instrument approach and departure procedures at the airport, and for the safety and management of IFR operations within the National Airspace System.
Proposed Amendment of Air Traffic Service (ATS) Route Q-5; Western United States
Document Number: 2018-05584
Type: Proposed Rule
Date: 2018-03-21
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend United States Area Navigation (RNAV) route Q-5 in the western United States. The route will now terminate at a waypoint (WP) that connects to an Oakland International Airport (OAK), Standard Terminal Arrival Route (STAR) near Oakland CA.