Department of Transportation May 28, 2015 – Federal Register Recent Federal Regulation Documents

This action proposes special conditions for the Pratt and Whitney Canada PW210A engine model. This engine will have a novel or unusual design featurean additional one engine inoperative (OEI) rating that combines the 30-second and 2-minute OEI ratings into a single rating. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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 notice announces renewal of National Freight Advisory Committee's charter for a period of 1 year (NFAC), effective May 28, 2015. The NFAC will provide information, advice, and recommendations to the U.S. Secretary of Transportation on matters relating to U.S. freight transportation.

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.

We propose to adopt a new airworthiness directive (AD) for certain Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 188 series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) indicating that a certain circumferential fuselage splice is subject to widespread fatigue damage (WFD). This proposed AD would require an inspection for corrosion and previous repairs, severed stringers, cracking, and loose or distressed fasteners of the forward and aft ends of the stringer splices of certain stringers, inspection for cracking and modification of certain fastener holes common to the stringer and splice member at the forward and aft ends of the splice, and related investigative and corrective actions if necessary. We are proposing this AD to prevent loss of residual strength of a certain circumferential fuselage splice, which could lead to rapid decompression of the cabin and potential loss of the airplane.

In accordance with the Paperwork Reduction Act of 1995, FMCSA announces its plan to submit the Information Collection Request (ICR) described below to the Office of Management and Budget (OMB) for its review and approval and invites public comment. The Agency is asking OMB to renew without change FMCSA's estimate of the paperwork burden imposed by its regulations pertaining to the training of certain entry- level drivers of commercial motor vehicles (CMVs). Since 2004, FMCSA regulations have prohibited the operation of certain CMVs by individuals with less than 1 year of CMV-driving experience until they obtain this training.

This action would revise the FAA's requirements for an application to operate in Reduced Vertical Separation Minimum (RVSM) airspace. This proposal would eliminate the burden and expense of developing, processing, and approving RVSM maintenance programs. As a result of this proposed revision, an applicant to operate in RVSM airspace would no longer be required to develop and submit an RVSM maintenance program solely for the purpose of an RVSM authorization. Because of other, independent FAA airworthiness regulations, all aircraft operators would nevertheless continue to be required to maintain RVSM equipment in an airworthy condition.

FRA hereby gives notice that it is submitting the following Information Collection request (ICR) to the Office of Management and Budget (OMB) for emergency processing under the Paperwork Reduction Act of 1995. FRA requests that OMB authorize the collection of information identified below by May 26, 2015, for a period of 180 days.

FRA is issuing this emergency order (EO or Order) to require that the National Railroad Passenger Corporation (Amtrak) take actions to control passenger train speed at certain locations on main line track in the Northeast Corridor (as described by 49 U.S.C. 24905(c)(1)(A)). Amtrak must immediately implement code changes to its Automatic Train Control (ATC) System to enforce the passenger train speed limit ahead of the curve at Frankford Junction in Philadelphia, Pennsylvania, where a fatal accident occurred on May 12, 2015. Amtrak must also identify each main track curve on the Northeast Corridor where there is a significant reduction (more than 20 miles per hour (mph)) from the maximum authorized approach speed to those curves for passenger trains. Amtrak must then develop and comply with an FRA- approved action plan to modify its existing ATC System or other signal systems (or take alternative operational actions) to enable enforcement of passenger train speed limits at the identified curves. Amtrak must also install additional wayside passenger train speed limit signage at appropriate locations on its Northeast Corridor right-of-way.

We are superseding airworthiness directive (AD) 2014-01-01 for all Turbomeca S.A. Arrius 2F turboshaft engines. AD 2014-01-01 required a one-time inspection of the ejector assembly nozzle of certain serial number (S/N) lubricating devices and, if a discrepancy was found, removal and replacement of the affected ejector assembly nozzle with a part eligible for installation. This AD requires the same action as AD 2014-01-01 and expands the list of affected S/N lubricating devices. This AD was prompted by the determination that additional lubricating devices, identifiable by S/N, may have an incorrect bonding of the nozzle on the ejector assembly. We are issuing this AD to prevent failure of the ejector assembly nozzle, which could lead to an in- flight shutdown (IFSD) of the engine, damage to the engine, and damage to the helicopter.

We are superseding Airworthiness Directive (AD) 2014-20-11, for Zodiac Seats France 9140, 9166, 9173, 9174, 9184, 9188, 9196, 91B7, 91B8, 91C0, 91C2, 91C4, 91C5, 91C9, 9301, and 9501 series passenger seat assemblies. AD 2014-20-11 required a general visual inspection for cracking of backrest links; replacement with new links if cracking is found; and eventual replacement of all links with new links. This AD was prompted by a determination that a model designation specified in paragraph (c)(1) of that AD was incorrect. This new AD identifies the correct model designation. We are issuing this AD to detect and correct cracks in the backrest links, which could affect the structural integrity of seat backrests. Failure of the backrest links could result in injury to an occupant during emergency landing conditions.