Department of Transportation October 27, 2009 – Federal Register Recent Federal Regulation Documents

The Federal Transit Administration (FTA), in cooperation with the Orange County Transportation Authority (OCTA) and the City of Anaheim, is planning to prepare a Draft Environmental Impact Statement/ Environmental Impact Report (DEIS/EIR) to provide transit service over a 3.5-mile corridor between the future ARTIC on the east and The Anaheim Resort on the west. The EIS will be prepared in accordance with regulations implementing the National Environmental Policy Act (NEPA) as well as provisions of the Safe, Accountable, Flexible, and Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU, 2005). The purpose of this Notice of Intent is to alert interested parties regarding the plan to prepare the DEIS, to provide information on the proposed transit project, to invite participation in the EIS process, including comments on the scope of the DEIS proposed in this notice, and to announce that public scoping meetings will be conducted.

The FHWA is issuing this notice to announce actions taken by FHWA and other Federal agencies that are final within the meaning of 23 U.S.C. Section 139(l)(1). The actions relate to the Highway 1 Soquel to Morrissey Auxiliary Lanes Project in the City of Santa Cruz, and Santa Cruz County, California. The project would include the following: Adding auxiliary lanes to Highway 1 between the interchanges of Soquel Avenue and Morrissey Boulevard for a distance of less than one mile; replacing the La Fonda overcrossing while providing wider sidewalks and new bike lanes; providing sidewalk improvements at Rooney Street and Morrissey Boulevard west of Pacheco Avenue; and installing a raised crosswalk at the south end of the La Fonda Bridge near the entrance to Harbor High School.

The FAA is revising an existing airworthiness directive (AD), which applies to all Airbus Model A300 airplanes. That AD currently requires revising the Airworthiness Limitations Section of the Instructions for Continued Airworthiness to incorporate new limitations for fuel tank systems. This AD clarifies the intended effect of the AD on spare and on-airplane fuel tank system components. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors caused by latent failures, alterations, repairs, or maintenance actions, could result in fuel tank explosions and consequent loss of the airplane.

This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

The FAA is superseding an existing airworthiness directive (AD) for Hartzell Propeller Inc. ()HC-()2Y()-() series propellers with non-suffix serial number (SN) propeller hubs installed on Lycoming O-, IO-, LO-, and AEIO-360 series reciprocating engines. That AD currently requires initial and repetitive eddy current inspections (ECIs) of the front cylinder half of the propeller hub for cracks and removing cracked hubs from service before further flight. In addition, that AD allows installation of an improved design propeller hub (suffix SN ``A'' or ``B'') as terminating action to the repetitive ECI. This ad requires the same actions but changes the affected propeller series designation to ()HC-()2Y(K,R)-() series propellers with non-suffix SN propeller hubs and suffix SN letter ``E'' propeller hubs. This AD also expands the engine eligibility to include Lycoming LIO-, TO-, LTO-, AIO-, and TIO-360-series engines. This AD results from the need to make changes to the affected series designation of propellers, to expand the engine applicability, and to respond to comments received on AD 2006- 18-15. We are issuing this AD to prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control.

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

We are adopting a new airworthiness directive (AD) for certain Airbus model series airplanes listed above. This AD requires revising the Airworthiness Limitations Section of the Instructions for Continuing Airworthiness to incorporate new fuel system limitations for airplanes modified in accordance with Supplemental Type Certificate (STC) ST00092BO. This AD also requires a general visual inspection for tank unit separation and compensator separation of the center, inner, and outer fuel tanks, and trim fuel tanks of the tank units, and corrective actions if necessary. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent a potential of ignition sources inside fuel tanks, which in combination with flammable fuel vapors, could result in a fuel tank fire or explosion and consequent loss of the airplane.