Department of Transportation December 24, 2015 – Federal Register Recent Federal Regulation Documents
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Pipeline Safety: Request for Special Permit
Pursuant to the Federal pipeline safety laws, PHMSA is publishing this notice of a special permit request we have received from a pipeline operator, seeking relief from compliance with certain requirements in the Federal pipeline safety regulations. This notice seeks public comments on this request, including comments on any safety or environmental impacts. At the conclusion of the 30-day comment period, PHMSA will evaluate the request and determine whether to grant or deny a special permit.
Notice of Intent To Rule on Request To Release Lake Murray State Park Airport at Ardmore, Oklahoma
The FAA proposes to rule and invites public comment on the release of Lake Murray State Park Airport at Lake Murray State Park in Ardmore, Oklahoma.
Annual Random Controlled Substances Testing Percentage Rate for Calendar Year 2016
The FMCSA announces, pursuant to 49 CFR 382.305, that it is reducing the minimum annual percentage rate for random controlled substances testing for drivers of commercial motor vehicles (CMVs) requiring a commercial driver's license (CDL) from the current rate of 50 percent of the average number of driver positions to 25 percent of the average number of driver positions, effective in calendar year 2016. The FMCSA Administrator has the discretion to decrease the minimum annual random testing percentage rate based on the reported positive random test rate for the entire motor carrier industry. Based on the controlled substances random test data in FMCSA's Management Information System (MIS) for calendar years 2011, 2012, and 2013, the positive rate for controlled substances random testing fell below the 1.0 percent threshold for 3 consecutive calendar years. As a result, the Agency will lower the controlled substances minimum annual percentage rate for random controlled substances testing to 25 percent of the average number of driver positions. In accordance with 49 CFR 382.305(e)(2) if, in the future, the reported positive rate for any calendar year is equal to or greater than 1.0 percent, the FMCSA Administrator will increase the minimum annual percentage rate for random controlled substances testing to 50 percent of all driver positions.
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 120 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.
Pipeline Safety: Random Drug Testing Rate; Contractor Management Information System Reporting; and Obtaining Drug and Alcohol Management Information System Sign-In Information
PHMSA has determined that the minimum random drug testing rate for covered employees will remain at 25 percent during calendar year 2016. Operators are reminded that drug and alcohol testing information must be submitted for contractors performing or ready to perform covered functions. For calendar year 2015 reporting, PHMSA will not attempt to mail the ``user name'' and ``password'' for the Drug and Alcohol Management Information System (DAMIS) to operators, but will make the user name and password available in the PHMSA Portal (https:// portal.phmsa.dot.gov/pipeline).
Potential Benefits and Feasibility of Voluntary Compliance; Public Listening Sessions
The FMCSA announces that it will hold two public listening sessions, on January 12 and 31, 2016, to solicit information on the potential benefits and feasibility of voluntary compliance and ways to credit carriers and drivers who initiate and establish programs that promote safety beyond the standards established in FMCSA regulations. The recently enacted Fixing America's Surface Transportation (FAST) Act mandates that the FMCSA Administrator allow recognition for a motor carrier that installs advanced safety equipment, enhanced driver fitness measures, fleet safety management tools, technologies, and programs and other standards for use by motor carriers to receive recognition, including credit or an improved Safety Measurement System (SMS) percentile. FMCSA is soliciting comment to develop a process for identifying and reviewing these opportunities to provide credit to those carriers and drivers who go above and beyond the regulatory requirements. The listening sessions are intended to provide interested parties with an opportunity to share their views on this topic with Agency representatives, along with any data or analysis they may have. All comments will be transcribed and placed in the docket referenced above for FMCSA's consideration. The entire proceedings of both meetings will be webcast.
Deepwater Port License Application: Delfin LNG LLC, Delfin LNG Deepwater Port
The Maritime Administration (MARAD), in cooperation with the U.S. Coast Guard (USCG), announces the receipt and availability of the amended deepwater port license application submitted by Delfin LNG LLC (Delfin LNG) on November 19, 2015 (amended application). The purpose of this Federal Register Notice is to explain the changes between the original application and the amended application and seek public comments regarding the amended application. Please note, MARAD and USCG have determined that this Federal Register Notice is sufficient for satisfying National Environmental Policy Act (NEPA) requirements for public scoping and seeking public comment on an agency action. As such, no public scoping meetings are planned to be held for the Delfin LNG amended application. A Notice of Application that summarized the original Delfin LNG license application was published in the Federal Register on July 16, 2015 (80 FR 42162). A Notice of Intent to Prepare an Environmental Impact Statement and Notice of Public Meetings was published in the Federal Register on Wednesday, July 29, 2015 (80 FR 45270). This Notice incorporates the aforementioned Notices by reference and highlights changes to the proposed Delfin LNG project made since the original application was deemed complete. The proposed Delfin LNG deepwater port incorporates onshore components, which are subject to the jurisdiction of the Federal Energy Regulatory Commission (FERC). These facilities are described in the section of this notice titled ``FERC Application.''
Deepwater Port License Application: Liberty Natural Gas LLC, Port Ambrose Deepwater Port; Withdrawal of Application and Termination of Federal Application Review Process
The Maritime Administration (MARAD) announces the termination of the Liberty Natural Gas LLC (Liberty) Port Ambrose Deepwater Port License Application and all related Federal processing activities required by applicable provisions of the Deepwater Port Act of 1974, as amended (Act). On September 28, 2015, Liberty submitted to MARAD and the U.S. Coast Guard (USCG) an application under the Act for a license and all Federal authorizations required to own, construct, and operate a deepwater port for the importation of liquefied natural gas (LNG) into the United States. The deepwater port, known as Port Ambrose, was proposed to be located in the offshore waters of New York and New Jersey, in the New York Bight. On June 14, 2013, MARAD and USCG deemed the application complete, designated New York and New Jersey as adjacent coastal states (ACS) and commenced the Federal application review process required under the Act. This process also included a comprehensive environmental assessment, public meetings and coordination of the application review process with relevant Federal and State agencies. Upon completion of the environmental review process required by the National Environmental Policy Act (NEPA) and the final public licensing hearings, Governor Andrew M. Cuomo of the State of New York, notified the Maritime Administration, by letter dated November 12, 2015, of his disapproval of the Liberty Port Ambrose deepwater port project. Governor Cuomo's disapproval was issued in accordance with the provisions outlined in 33 U.S.C. Section 1508(c)(8) which state, the Secretary (or Maritime Administrator by delegated authority) may issue a deepwater port license only if the Governor of the ACS approves or is presumed to approve, issuance of the license. In light of Governor Cuomo's disapproval of the application, Liberty notified MARAD, by letter dated November 18, 2015, of its withdrawal of the Port Ambrose license application from the Federal review process. As a consequence of Liberty's withdrawal of its application, the Federal application review process and all related Federal processing activities were terminated on November 18, 2015. This Federal Register Notice shall serve as official announcement to the public that the Federal review and processing of the Liberty Port Ambrose deepwater port license application is terminated.
Proposed Establishment of Class E Airspace; Danville, AR
This action proposes to establish Class E airspace at Danville, AR. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures developed at Danville Municipal Airport, for the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Airworthiness Directives; Fokker Services B.V. Airplanes
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 cracking in a certain section of the secondary structure of the wing. This proposed AD would require a one-time inspection of the trailing edge rib, and corrective action if necessary. We are proposing this AD to detect and correct cracking that could lead to failure of the affected rib and consequent reduced control of the airplane.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to supersede Airworthiness Directive (AD) 2014-16- 02, for certain Bombardier, Inc. Model CL-600-1A11 (CL-600) airplanes. AD 2014-16-02 currently requires revising the airplane flight manual to prohibit thrust reverser operation, doing repetitive detailed inspections of both engine thrust reversers for cracks, and modifying the thrust reversers if necessary. The modification of the thrust reversers is also an optional terminating action for the repetitive inspections. Since we issued AD 2014-16-02, we have determined that it is necessary to add a requirement to repair or modify the thrust reversers, which would terminate the requirements of AD 2014-16-02. We are proposing this AD to detect and correct cracks of the translating sleeve at the thrust reverser actuator attachment points, which could result in deployment or dislodgement of an engine thrust reverser in flight and subsequent reduced control of the airplane.
Airworthiness Directives; B-N Group Ltd. Airplanes
We propose to adopt a new airworthiness directive (AD) for B-N Group Ltd. Models BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN- 2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN- 2B-26, BN-2B-27, BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3 BN2A, BN2B, and BN2A MKIII (all models on TCDS A17EU and A29EU) airplanes that would supersede AD 2007-06-06. 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 cracks in the inner shell of certain pitot/static pressure heads. We are issuing this proposed AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 777 airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the lap splices of the aft pressure bulkhead webs are subject to widespread fatigue damage (WFD) on aging Model 777 airplanes that have accumulated at least 38,000 total flight cycles. This AD requires repetitive inspections for any crack in the aft webs of the radial lap splices of the aft pressure bulkhead, and, if necessary, corrective actions. We are issuing this AD to detect and correct fatigue cracking in the aft webs of the radial lap splices of the aft pressure bulkhead; such cracking could result in reduced structural integrity of the airplane, decompression of the cabin, and collapse of the floor structure.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-200, A330-200 Freighter, and A330-300 series airplanes; and all Model A340-200 and A340-300 series airplanes. This AD was prompted by reports that a bracket that attaches the cockpit instrument panel to the airplane structure does not sustain the fatigue loads of the design service goal. This AD requires repetitive inspections of that bracket for cracking and to determine if both lugs are fully broken, an inspection for cracking of an adjacent bracket if necessary, and corrective actions if necessary. This AD also provides an optional modification, which terminates the repetitive inspections. We are issuing this AD to detect and correct cracking on a bracket of the cockpit instrument panel, which, combined with failure of the horizontal beam, could lead to collapse of the cockpit panel, and reduced controllability of the airplane.
Airworthiness Directives; Bombardier, Inc. Airplanes
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes. This AD was prompted by a report of an aft equipment bay fire due to chafing and subsequent arcing of the integrated drive generator (IDG) power cables. Additionally, we have received several reports of broken support brackets of the hydraulic line. This AD requires a one-time inspection of the IDG power cables for chafing, and for any cracked or broken support bracket of the hydraulic line; and corrective actions if necessary. We are issuing this AD to detect and correct broken support brackets of the hydraulic lines, which could result in inadequate clearance between the IDG power cables and hydraulic lines and chafing of the IDG power cables, and consequent high energy arcing and an uncontrolled fire in the aft equipment bay.
Airworthiness Directives; The Boeing Company Airplanes
We are superseding Airworthiness Directive (AD) 2013-23-03, which applies to certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes. AD 2013-23-03 required a detailed inspection of certain attach fittings for a cylindrical defect, and replacement if necessary. For certain airplanes, this new AD requires new inspections of the inboard actuator attach fittings for machining defects, and overhaul or replacement if necessary. This new AD also limits the compliance time for doing the replacement for certain other airplanes. This AD was prompted by a report that a machining defect was also found on some of the actuator assemblies inspected during manufacture. This defect could lead to fatigue cracking and subsequent fracture. We are issuing this AD to detect and correct defective inboard actuator attach fittings which, combined with loss of the outboard actuator load path, could result in uncontrolled retraction of the outboard flap, damage to flight control systems, and consequent reduced controllability of the airplane.
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
We are revising an earlier proposed airworthiness directive (AD) for all Gulfstream Aerospace Corporation Model GV and GV-SP airplanes. The NPRM proposed to supersede Airworthiness Directive (AD) 2013-22-19, which requires inspecting to determine if fuel boost pumps having a certain part number are installed, replacing the fuel boost pumps having a certain part number, and revising the airplane maintenance or inspection program to include revised instructions for continued airworthiness. The NPRM also proposed to require revising the airplane maintenance program to include a fuel leak check of the fuel boost pumps, using new service information. The NPRM was prompted by reports of two independent types of failure of the fuel boost pump: overheat damage on the internal components and external housing, and fuel leakage. This action revises the NPRM by reducing the compliance time for revising the airplane maintenance program. We are proposing this supplemental NPRM (SNPRM) to prevent fuel leakage in combination with a capacitor clearance issue, which could result in an uncontrolled fire in the wheel well. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
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