Department of Transportation October 14, 2015 – Federal Register Recent Federal Regulation Documents

This action amends Restricted Areas R-3602A and R-3602B, Manhattan, KS, to accurately identify the R-3602A and R-3602B boundary segments described using the Chicago, Rock Island and Pacific Railroad right-of-way, the R-3602A and R-3602B shared boundary segment described using Old U.S. Highway 77, and the R-3602A and Riley Military Operations Area (MOA) shared boundary segment described using the Milford Reservoir shoreline. The restricted area ceilings are also amended to be expressed as flight levels (FL), the Marshall Army Air Field Radio Beacon (RBN) referenced in R-3602B is changed to the Cavalry Nondirectional Beacon (NDB), and the restricted areas using agency information is updated to include the military service of the using agency. This action does not affect the overall restricted area boundaries, designated altitudes, times of designation, or activities conducted within the restricted areas. Additionally, boundary segment amendments of the Riley MOA, ancillary to the restricted area amendments, are being made. Since the R-3602A and R-3602B restricted areas share boundaries with the Riley MOA, the FAA included discussion of the Riley MOA amendments in this rule. Lastly, the MOA using agency is being amended to match the restricted areas using agency information.

BMW of North America, LLC, (BMW) a subsidiary of BMW AG in Munich, Germany, has determined that certain model year (MY) 2014 BMW 7 series and 6 series vehicles do not fully comply with paragraph S5.2.1 of Federal Motor Vehicle Safety Standard (FMVSS) No. 101, Controls and Displays. BMW has filed an appropriate report dated December 5, 2013 pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports.

This notice is to advise interested persons of two public meetings occurring on Thursday, November 12, 2015, both held at the Department of Transportation (DOT) headquarters. PHMSA will conduct a public meeting to discuss proposals in preparation for the 48th session of the United Nations Sub-Committee of Experts on the Transport of Dangerous Goods (UNSCOE TDG), to be held November 30 to December 09, 2015, in Geneva, Switzerland. During this meeting, PHMSA is also requesting comments relative to potential new work items that may be considered for inclusion in its international agenda. Also on Thursday, November 12, 2015, the Occupational Safety and Health Administration (OSHA) will conduct a public meeting (Docket No. OSHA-H022k-2006-0062) to discuss proposals in preparation for the 30th session of the United Nations Sub-Committee of Experts on the Globally Harmonized System of Classification and Labelling of Chemicals (UNSCEGHS), to be held December 9 to December 11, 2015, in Geneva, Switzerland. Time and Location: Both the PHMSA and OSHA public meetings will take place on Thursday, November 12, 2015 at the DOT Headquarters in the West Building, which is located at 1200 New Jersey Avenue SE., Washington, DC 20590-0001. The times are:

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Models PA-28-161, PA-28-181, and PA-28R-201 airplanes. This AD requires inspecting the right wing rib at wing station 140.09 for cracks and taking necessary corrective action. This AD was prompted by a report of cracks found in the wing rib bead radius that were formed during production. We are issuing this AD to correct the unsafe condition on these products.

We are superseding airworthiness directive (AD) 2014-14-02 for certain Pratt & Whitney Canada Corp. (P&WC) PW120, PW121, PW121A, PW124B, PW127, PW127E, PW127F, PW127G, and PW127M turboprop engines. AD 2014-14-02 required removal of the O-ring seal from the fuel manifold fitting. This new AD requires replacement of the fuel nozzle and the fuel manifold flow adapter. This AD was prompted by reports of fuel leaks at the interface between the fuel manifold and the fuel nozzle that resulted in engine fire. We are issuing this AD to correct the unsafe condition on these products.

We are adopting a new airworthiness directive (AD) for Schempp-Hirth Flugzeugbau GmbH Models Duo Discus and Duo Discus T powered sailplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued 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 excessive load on the air brake system. We are issuing this AD to require actions to address the unsafe condition on these products.