Department of Transportation 2014 – Federal Register Recent Federal Regulation Documents

We are adopting a new airworthiness directive (AD) for certain Saab AB, Saab Aerosystems Model SAAB 2000 airplanes. This AD was prompted by a report of rudder pedal restriction which was the result of water leakage at the inlet tubing of an in-line heater in the lower part of the forward fuselage. This AD requires deactivating the potable water system, or alternatively filling and activating the potable water system. We are issuing this AD to prevent rudder pedal restriction due to the pitch control mechanism becoming frozen as the result of water spray, which could prevent disconnection and normal pitch control, and consequently result in reduced controllability of the airplane.

We propose to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This proposed AD was prompted by a report of two cases of heavy (hard to move) aileron control caused by aileron cables stuck in a clump of ice in the wheel bay. This proposed AD would require installing drain tubes on the center wing rear spar. We are proposing this AD to prevent accumulated water near or on the aileron control cables, which could freeze and result in reduced control of the airplane.

The FHWA is issuing this notice to advise the public that an environmental impact statement (EIS) will be prepared for a proposed Northwest Corridor highway project within the Municipalities of Hatillo, Camuy, Quebradillas, Isabela, Moca and Aguadilla in the Commonwealth of Puerto Rico.

The CMAQ program provides funding to State and local governments for transportation projects and programs to help meet the requirements of the Clean Air Act (CAA). Funding is available to reduce congestion and improve air quality for areas that do not meet the National Ambient Air Quality Standards (NAAQS) for ozone, carbon monoxide (CO), or particulate matter (nonattainment areas) and for areas that were out of compliance but have now met the standards (maintenance areas). The Moving Ahead for Progress in the 21st Century Act (MAP-21) requires priority use of CMAQ funds in areas that are designated nonattainment or maintenance for fine particulate matter (PM2.5) NAAQS under the CAA. Specifically, an amount equal to 25 percent of the CMAQ funds apportioned to each State for a nonattainment or maintenance area that is based all or in part on the weighted population of the PM2.5 nonattainment area shall be obligated to projects that reduce PM2.5 emissions in such area. These projects include diesel retrofits for on-road and some off- road applications, as well as for diesel equipment operated on a highway construction project within PM2.5 nonattainment and maintenance areas. Although the MAP-21 language for the CMAQ funds that must be obligated for PM2.5 projects (referred to in this NPRM as a ``set-aside'') instructs that the set-aside be calculated based on ``weighted population'' for PM2.5, the statute does not specify the values to be applied to determine the weighted population. In this proposed rule, FHWA is requesting comments on a proposed weighting factor of 5, to be used in determining the weighted population of a PM2.5 nonattainment area.

These special conditions are issued for Airbus Model A350-900 airplanes. These airplanes have a novel or unusual design feature associated with control-surface awareness and mode annunciation provided by the electronic flight-control system. 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.

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 approval and invites public comment. The FMCSA requests approval to revise and renew an ICR entitled, ``Commercial Driver Licensing and Test Standards,'' due to an increase in the number of Commercial Driver License Information System (CDLIS) driver records from 12.8 to 14.6 million and the addition of one information collection item: ``Driver completion of knowledge and skills tests [49 CFR 383.71(a)(2)(ii) and (b)(2)].'' This ICR is needed to ensure that drivers, motor carriers and the States are complying with notification and recordkeeping requirements for information related to testing, licensing, violations, convictions and disqualifications and that the information is accurate, complete and transmitted and recorded within certain time periods as required by the Commercial Motor Vehicle Safety Act of 1986 (CMVSA), as amended.

We propose to adopt a new airworthiness directive (AD) for all Pacific Aerospace Limited Model 750XL airplanes that would supersede AD 2014-04-03. This proposed 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 broken control column attachment bolts failing in service. We are issuing this proposed AD to require actions to address the unsafe condition on these products.

We are superseding Airworthiness Directive (AD) 2003-18-10 for certain The Boeing Company Model 767 airplanes. AD 2003-18-10 required revising the Airworthiness Limitations Section of the maintenance planning data (MPD) document. This new AD also requires revising the maintenance program to incorporate an additional limitation, which terminates the existing requirements; and adds airplanes to the applicability. This AD was prompted by a re-evaluation of certain doors and flaps based on their fatigue-critical nature. We are issuing this AD to detect and correct fatigue cracking of the principal structural elements (PSEs), which could adversely affect the structural integrity of the airplane.

We are adopting a new airworthiness directive (AD) for certain Airbus Model A319-111, -112, -115, -132, and -133 airplanes; Model A320-214, -232, and -233 airplanes; and Model A321-211, -231, and -232 airplanes. This AD requires a detailed inspection for missing fasteners on the frame between certain stringers; for certain airplanes, a rototest inspection of the fastener holes for cracking; and corrective actions if necessary. This AD was prompted by a report that when the cabin lining was removed during a cabin conversion it was discovered that fasteners were missing on the frame. We are issuing this AD to detect and correct missing fasteners which, if not corrected, could affect the structural integrity of the airframe and could result in rapid decompression.

PMHSA is issuing this ANPRM in conjunction with a notice of proposed rulemaking (NPRM)Hazardous Materials: Enhanced Tank Car Standards and Operational Controls for High-Hazard Flammable Trains (2137-AE91), which PHMSA is also publishing today. In this ANPRM, PHMSA, in consultation with the Federal Railroad Administration (FRA), seeks comment on potential revisions to its regulations that would expand the applicability of comprehensive oil spill response plans (OSRPs) to high-hazard flammable trains (HHFTs) based on thresholds of crude oil that apply to an entire train consist.

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-2D24 (Regional Jet Series 900) airplanes, and Model CL- 600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by two in-service reports of fracture of the rudder pedal tubes installed on the pilot-side rudder bar assembly. This AD requires repetitive inspections for cracking and damage of the pilot-side rudder pedal tubes, and corrective action if necessary. This AD also provides optional terminating action for the repetitive inspections. We are issuing this AD to detect and correct cracked and damaged pilot-side rudder pedal tubes, which could result in loss of function of the pilot's rudder pedal during flight, takeoff, or landing, and could result in reduced controllability of the airplane.

This action proposes special conditions for the SNECMA, Silvercrest-2 SC-2D engine model. This engine will have a novel or unusual design featurean additional takeoff rating that increases the exhaust gas temperature (EGT) limit to maintain takeoff thrust in certain high ambient temperature conditions with one engine inoperative (OEI) for a maximum of 10 minutes. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. The 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.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval for to renew an information collection. FAA Form 7480-1 (Notice of Landing Area Proposal) is used to collect information about any construction, alteration, or change to the status or use of an airport.

This notice states the reasons for denying a Defect Petition (DP) (DP 13-002) submitted under 49 CFR parts 552 by Ms. Jessie A. Powell of Middleboro, MA (petitioner) in a January, 2013 letter to the Administrator of NHTSA (the ``Agency''). The petitioner requested that the Agency open an investigation into software and brake failures on model year (MY) 2012 Toyota Prius C vehicles (the ``Subject Vehicles''). After reviewing materials in-hand, those furnished by the petitioner, and upon completing an inspection of her vehicle, NHTSA sees no indication that additional investigation would lead to a finding that a defect related to motor vehicle safety exists. NHTSA has concluded that further investigation of the issue raised in the petition is not warranted. The Agency accordingly has denied the petition.

This document proposes fees for Fiscal Year 2015 and until further notice relating to the registration of importers and the importation of motor vehicles not certified as conforming to the Federal motor vehicle safety standards (FMVSS). These fees are needed to maintain the registered importer (RI) program.

This notice disposes of public comments received by the Federal Aviation Administration (FAA) in response to a Federal Register notice published on February 22, 2013, requesting comments on a potential restructuring of the rotorcraft airworthiness standards of Title 14 of the Code of Federal Regulations (14 CFR) parts 27 (normal category rotorcraft) and 29 (transport category rotorcraft). Specifically, the agency sought comments on the necessity of updates to parts 27 and 29, including whether to change the existing weight- and seat-based applicability standards for normal and transport rotorcraft. Based on the comments received, the FAA is terminating this docket. Commenters indicated a substantial interest in revising or restructuring the certification standards for parts 27 and 29, and the FAA's Rotorcraft Directorate will begin establishing the appropriate forums to involve interested parties.

We propose to supersede airworthiness directive (AD) 2010-21- 07 for Eurocopter France (now Airbus Helicopters) Model AS350B3 and EC130B4 helicopters. AD 2010-21-07 currently requires inspecting the pilot's and co-pilot's throttle twist for proper operation of the contactors. This proposed AD would retain the requirements of AD 2010- 21-07, include additional inspection procedures, and revise the inspection interval. These proposed actions are intended to prevent unintended touchdown during a practice autorotation at a flight-idle power setting, damage to the helicopter, and injury to occupants.

We propose to adopt a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 430 helicopters to require inspecting the tail rotor control tube assembly (control tube) and either repairing or replacing the control tube. This proposed AD is prompted by two reports of failure of the control tube bonded clevis. The proposed actions are intended to prevent failure of a control tube bonded clevis, which could lead to failure of the control tube and subsequent loss of helicopter control.

In accordance with the Paperwork Reduction Act of 1995, PHMSA invites public comments on our intent to request the Office of Management and Budget's approval to revise and renew an information collection currently under OMB Control Number 2137-0596 titled: ``National Pipeline Mapping System Program.'' The collection currently requires operators to submit geospatial data, attributes, metadata, public contact information and a transmittal letter to the National Pipeline Mapping System (NPMS) program. The proposed revisions will require operators to submit additional information to the NPMS.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 2, 2014, vol. 79, no. 85, pages 25170-25171. The FAA/ AST will collect lessons learned from members of the commercial space industry in order to carry out the safety responsibilities in 49 U.S.C. Chapter 701 Section 70103(c).

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval for a new information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on August 12, 2013, vol. 78, no. 155, pages 48925-48926. The FAA Modernization and Reform Act of 2012 included a mandate to begin collection of operational data from Air Ambulance operators. The Act mandates that not later than 2 years after the date of enactment, and annually thereafter, the Administrator shall submit to the Committee on Transportation and Infrastructure of the House of Representatives and the Committee on Commerce, Science, and Transportation of the Senate, a report containing a summary of the data collected. The FAA received a total of 17 responses to the request for public comment. Based on the comments, the FAA has made adjustments in the reporting requirements, frequency of reporting and the format for submission. Specifically, the linkage among the registration number, time of day, flight time, IFR flight time, and base has been removed. Reporting requirements have changed from a ``per flight'' basis to an aggregate basis. Additionally, the reporting requirement has been reduced from a quarterly report to an annual report.