Department of Transportation July 16, 2018 – Federal Register Recent Federal Regulation Documents

The FAA proposes to add a new load condition to the design standards for transport category airplanes. The new load condition would require the airplane be designed to withstand the loads caused by rapid reversals of the rudder pedals and would apply to transport category airplanes that have a powered rudder control surface or surfaces. This rule is necessary because accident and incident data show that pilots sometimes make rudder reversals during flight, even though such reversals are unnecessary and discouraged by flightcrew training programs. The current design standards do not require the airplane structure to withstand the loads that may result from such reversals. If the airplane loads exceed those for which it is designed, the airplane structure may fail, resulting in catastrophic loss of control of the airplane. This proposal aims to prevent structural failure of the rudder and vertical stabilizer that may result from these rudder reversals.

The FHWA and the State of Nebraska, acting by and through its Department of Transportation (State), propose participation of the State in the Categorical Exclusion Assignment program. This program allows FHWA to assign its authority and responsibility for determining whether certain designated activities within the geographic boundaries of the State, as specified in the proposed Memorandum of Understanding (MOU), are categorically excluded from preparation of an environmental assessment or an environmental impact statement under the National Environmental Policy Act.

These special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 series airplanes. This airplane will have a novel or unusual design feature when compared to the state of technology and design envisioned in the airworthiness standards for transport category airplanes. This design feature is a high incidence protection system that limits the angle of attack at which the airplane can be flown during normal low speed operation. 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.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

FRA proposes to eliminate the requirement that certain locomotives display a badge or tag to demonstrate the railroad has certified the locomotives comply with noise emission standards. This proposed rule would reduce economic burdens on the rail industry by removing the badge or tag requirement.