Department of Transportation February 19, 2013 – Federal Register Recent Federal Regulation Documents
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National Freight Advisory Committee
Pursuant to Section 9(a)(2) of the Federal Advisory Committee Act (FACA) (5 U.S.C., App. 2.), and in accordance with Title 41, Code of Federal Regulations, Section 102-3.65, and following consultation with the Committee Management Secretariat, General Services Administration, notice is hereby given that the NFAC will be established for a 2-year period. The Committee will provide advice and recommendations to the Secretary of Transportation on matters related to freight transportation in the United States, including: (1) Implementation of the freight transportation requirements of the Moving Ahead for Progress in the 21st Century Act (Pub. L. 112-141); (2) establishment of the National Freight Network; (3) development of a National Freight Strategic Plan; (4) development of strategies to help States implement State Freight Advisory Committees and State Freight Plans; (5) development of measures of conditions and performance in freight transportation; (6) development of freight transportation investment, data, and planning tools; and (7) legislative recommendations. Additionally, the establishment of the NFAC is necessary for the Department to carry out its mission and is in the public interest. The Committee will operate in accordance with the provisions of the FACA and the rules and regulations issued in implementation of that Act. This notice also requests nominations for members of the Committee to ensure a wide range of member candidates and a balanced Committee.
Agency Information Collection Activity; Notice of Request for Public Comment and Submission to OMB for Information Collection: Confidential Close Call Reporting for Transit Rail System
In accordance with the requirements of section 3506(c)(2)(A) of the Paperwork Reduction Act of 1995, BTS announces its plan to submit the Information Collection Request (ICR) described below to the Office of Management and Budget (OMB) for approval. On November 5, 2012, BTS published a Federal Register notice (77 FR 66502), allowing for a 60-day comment period on the ICR. The comment period closed on January 4, 2013. The agency received one comment, from the National Safety Council (NSC), Docket Comment RITA-2008-0002-0037, in response to the notice which supported the need for the information collection. The NSC comment stated they agreed with BTS that '' there is a need for proper data collection and analysis on close calls and other unsafe occurrences in the WMATA rail system.'' The purpose of this Notice is to allow 30 days for public comment to OMB on this collection from all interested individuals and organizations.
Special Conditions: Embraer S.A., Model EMB-550 Airplane; Landing Pitchover Condition
This action proposes special conditions for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with landing loads due to the automatic braking system. 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.
Special Conditions: Embraer S.A., Model EMB-550 Airplane; Interaction of Systems and Structures
These special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with the interaction of systems and structures. 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.
Special Conditions: Embraer S.A., Model EMB-550 Airplane; Electronic Flight Control System: Lateral-Directional and Longitudinal Stability and Low Energy Awareness
These special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with an electronic flight control system with respect to lateral-directional and longitudinal stability and low energy awareness. 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.
Special Conditions: Embraer S.A., Model EMB-550 Airplanes; Flight Envelope Protection: High Speed Limiting
These special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature, specifically an electronic flight control system which contains fly-by-wire control laws, including envelope protections, for the overspeed protection and roll limiting function. 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.
Qualification of Drivers; Exemption Applications; Vision
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 12 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemption renewals will provide a level of safety that is equivalent to or greater than the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Pilot Project on NAFTA Trucking Provisions
On September 12, 2011, FMCSA announced and requested public comment on data and information concerning the Pre-Authorization Safety Audit (PASA) for Grupo Behr de Baja California SA de CV (Grupo Behr), USDOT 861744, a motor carrier that applied to participate in the Agency's long-haul pilot program. That action was required by the ``U.S. Troop Readiness, Veterans' Care, Katrina Recovery, and Iraq Accountability Appropriations Act, 2007'' and all subsequent appropriations. While Grupo Behr successfully completed the PASA process, commenters raised concerns about the company's safety record. In addition, during the Agency's safety vetting process, an operating authority violation was discovered. As a result, the Agency placed Grupo Behr's application on hold. The purpose of this notice is to respond to the comments received in response to the September 12, 2011, notice, and to explain the enforcement action that the Agency took as a result of the operating authority violation. In addition, this notice advises that the Agency will now issue provisional authority to Grupo Behr for participation in the long-haul pilot program.
Special Conditions: Embraer S.A., Model EMB-550 Airplane; Design Roll Maneuver for Electronic Flight Controls
These special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with the design roll maneuver for electronic flight controls, specifically an electronic flight control system that provides control of the aircraft through pilot inputs to the flight computer. 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.
Special Conditions: Embraer S.A., Model EMB-550 Airplane, Limit Pilot Forces for Sidestick Control
These special conditions for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature, specifically sidestick controllers designed to be operated with only one hand. 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.
Special Conditions: Embraer S.A., Model EMB-550 Airplane; Electronic Flight Control System: Control Surface Awareness and Mode Annunciation
These special conditions are issued for the Embraer S.A. Model EMB-550 airplane. This airplane will have a novel or unusual design feature(s) associated with the control surface awareness and mode annunciation of 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.
Environmental Impact and Related Procedures
This final rule amends the Federal Highway Administration (FHWA) and Federal Transit Administration (FTA) joint procedures that implement the National Environmental Policy Act (NEPA) by enacting a new categorical exclusion (CE) for emergency actions as required by the Moving Ahead for Progress in the 21st Century Act (MAP-21). The final rule modifies the existing lists of FHWA and FTA CEs and expands the existing CE for emergencies to include emergency actions as described in MAP-21 and pursuant to this rulemaking.
Airworthiness Directives; Pratt & Whitney Canada Corp. Turboshaft Engines
We are adopting a new airworthiness directive (AD) for certain serial number Pratt & Whitney Canada Corp. PW206B, PW206B2, PW206C, PW207C, PW207D, PW207D1, PW207D2, and PW207E turboshaft engines. This AD was prompted by the discovery that certain power turbine (PT) disks were made to specific heat codes that may not achieve the maximum in- service life. This AD requires re-identification of the PT disk to a part number (P/N) with a lower life limit. We are issuing this AD to prevent possible uncontained PT disk failure and loss of helicopter control.
Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
We are superseding an existing airworthiness directive (AD) for all Pilatus Aircraft Ltd. Models PC-12, PC-12/45, PC-12/47, and PC- 12/47E airplanes. 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 a need to incorporate new revisions into the Limitations section, Chapter 4, of the FAA-approved maintenance program (e.g., maintenance manual). We are issuing this AD to require actions to address the unsafe condition on these products.
Aviation Rulemaking Advisory Committee; Meeting
The FAA is issuing this notice to advise the public of a meeting of the ARAC.
Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes
We are adopting a new airworthiness directive (AD) for all Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Gulfstream G150 airplanes. This AD was prompted by a review that determined that the runway slope and anti-ice corrections to V1 and take-off distances in the Gulfstream G150 Airplane Flight Manual (AFM) were presented in a non-conservative manner. This AD requires revising the performance section of the AFM to include procedures to advise the flightcrew of certain runway slope and anti-ice corrections and take-off distance values. We are issuing this AD to prevent the use of published non-conservative data, which could result in the inability to meet the required take-off performance, with consequent hazard to safe operation during performance-limited take-off operations.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes. This AD was prompted by reports of fuel leaking from the front spar of the wing through the slat track housing. This AD requires a detailed inspection of the inboard and outboard main slat track downstop assemblies and a torque application to the main track downstop assembly nuts of slat numbers 1 through 10, excluding the outboard track of slats 1 and 10; a detailed inspection of all slat track housings for foreign object debris (FOD) and visible damage; and corrective actions if necessary. We are issuing this AD to detect and correct incorrectly installed main slat track downstop assemblies, which, when the slat is retracted, could cause a puncture in the slat track housing and lead to a fuel leak and potential fire.
Airworthiness Directives; Pratt & Whitney Canada Corp Turboshaft Engines
We are adopting a new airworthiness directive (AD) for certain Pratt & Whitney Canada Corp. (P&WC) PT6C-67C turboshaft engines. This AD requires initial and repetitive borescope inspections to verify the presence of a retaining ring securing the power turbine (PT) baffle located near the second stage PT disk. If the engine fails the inspection, this AD also requires removing the engine from service before further flight. This AD was prompted by five reported incidents of second stage PT disk damage. We are issuing this AD to prevent damage to the PT disk which, if undetected, could cause uncontained PT disk failure and loss of control of the helicopter.
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