Department of Transportation May 14, 2013 – Federal Register Recent Federal Regulation Documents

Notice of Meeting of the Transit Rail Advisory Committee for Safety (TRACS)
Document Number: 2013-11516
Type: Notice
Date: 2013-05-14
Agency: Federal Transit Administration, Department of Transportation
This notice announces a public meeting of the Transit Rail Advisory Committee for Safety (TRACS). TRACS is a Federal Advisory Committee established by the U.S. Secretary of Transportation (the Secretary) in accordance with the Federal Advisory Committee Act to provide information, advice, and recommendations to the Secretary and the Federal Transit Administrator on matters relating to the safety of public transportation systems.
Operating Limitations at New York LaGuardia Airport
Document Number: 2013-11490
Type: Notice
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
This action amends the Order Limiting Operations at New York LaGuardia Airport (LGA) that published on December 27, 2006, and was amended on November 8, 2007, August 19, 2008, October 7, 2009, April 4, 2011, and May 23, 2012. The Order remains effective until the final Rule on Slot Management and Transparency for LaGuardia Airport, John F. Kennedy International Airport, and Newark Liberty International Airport becomes effective but not later than October 24, 2014.
Operating Limitations at Newark Liberty International Airport
Document Number: 2013-11489
Type: Notice
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
This action amends the Order Limiting Operations at Newark Liberty International Airport (EWR) that published on May 21, 2008, and was amended on October 7, 2009, and April 4, 2011. The Order remains effective until the final Rule on Slot Management and Transparency for LaGuardia Airport, John F. Kennedy International Airport, and Newark Liberty International Airport becomes effective but not later than October 24, 2014.
Operating Limitations at John F. Kennedy International Airport
Document Number: 2013-11467
Type: Notice
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
This action amends the Order Limiting Operations at John F. Kennedy International Airport (JFK) that published on January 18, 2008, and was amended on February 14, 2008, October 7, 2009, and April 4, 2011. The Order remains effective until the final Rule on Slot Management and Transparency for LaGuardia Airport, John F. Kennedy International Airport, and Newark Liberty International Airport becomes effective but not later than October 24, 2014.
Office of Commercial Space Transportation; Safety Approval Performance Criteria
Document Number: 2013-11438
Type: Notice
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA issued BST a safety approval, subject to the provisions of Title 51 U.S.C Subtitle V, ch. 509, and the orders, rules and regulations issued under it. Pursuant to Title 14 Code of Federal Regulations (14 CFR) Sec. 414.35, this Notice publishes the criteria that were used to evaluate the safety approval application. Background: BST applied for, and received, a safety approval for its ability to provide as a service, scenario based physiology training, which includes hypobaric chamber training. BST may offer its scenario based physiology altitude training as a service to a prospective launch and reentry operator to meet the applicable crew and participant training requirements of 14 CFR 460.5 and 14 CFR 460.51. Criteria Used To Evaluate Safety Approval Application: The performance criteria for this safety approval include 14 CFR 61.31(g) for additional training required for operating pressurized aircraft capable of operating at high altitudes. These criteria are FAA regulations, which are acceptable technical criteria for reviewing a safety approval application per 14 CFR 414.19(a)(1). The FAA's evaluation included assessment of BST's scenario based physiology training lesson plan and objectives, which include classroom and hypobaric chamber training for crew and space flight participants to experience and demonstrate knowledge of the following through testing: Understand fundamental principles of the atmosphere and how it relates to the human body. Understand the fundamentals of respiratory physiology and how it relates to hypoxia. Show competence in the identification of the many different symptoms and physical signs of hypoxia. Show advanced competence in the phenomena of neurological impairment (time of useful consciousness) due to hypoxia. Understand the effects of prolonged oxygen use. Understand the difference between decompression illness and hypoxia. Demonstrate using different scenarios the difference between slow decompression and rapid decompression. Identify personal symptoms of hypoxia and demonstrate donning of oxygen mask and ability to perform within a hypobaric chamber.
Petition for Waiver of Compliance
Document Number: 2013-11437
Type: Notice
Date: 2013-05-14
Agency: Federal Railroad Administration, Department of Transportation
Petition for Waiver of Compliance
Document Number: 2013-11436
Type: Notice
Date: 2013-05-14
Agency: Federal Railroad Administration, Department of Transportation
Petition for Waiver of Compliance
Document Number: 2013-11434
Type: Notice
Date: 2013-05-14
Agency: Federal Railroad Administration, Department of Transportation
Petition for Waiver of Compliance
Document Number: 2013-11432
Type: Notice
Date: 2013-05-14
Agency: Federal Railroad Administration, Department of Transportation
Nissan North America, Inc., Grant of Petition for Decision of Inconsequential Noncompliance
Document Number: 2013-11428
Type: Notice
Date: 2013-05-14
Agency: National Highway Traffic Safety Administration, Department of Transportation
Nissan North America, Inc. (Nissan), has determined that certain model year 2008 through 2010 Nissan Titan trucks do not fully comply with the requirements of paragraph S19.2.2(b) of Federal Motor Vehicle Safety Standard (FMVSS) No. 208, Occupant Crash Protection. Nissan has filed an appropriate report pursuant to 49 CFR Part 573, Defect and Noncompliance Responsibility and Reports, dated August 18, 2010. Pursuant to 49 U.S.C. 30118(d) and 30120(h) and the rule implementing those provision at 49 CFR Part 556, Nissan has petitioned for an exemption from the notification and remedy requirements of 49 U.S.C. Chapter 301 on the basis that this noncompliance is inconsequential to motor vehicle safety. Notice of receipt of Nissan's petition was published, with a 30 day public comment period, on December 21, 2010, in the Federal Register (75 FR 80109). No comments were received. To view the petition and all supporting documents log onto the Federal Docket Management System (FDMS) Web site at: https://www.regulations.gov/. Then follow the online search instructions to locate docket number ``NHTSA-2008-0210.'' Contact Information: For further information on this decision, contact Mr. Lawrence Valvo, Office of Vehicle Safety Compliance, the National Highway Traffic Safety Administration (NHTSA), telephone (202) 366-5359, facsimile (202) 366-7002. Vehicles Involved: Affected are approximately 102,254 model year 2008 through 2010 Nissan Titan trucks that were manufactured from April 10, 2007, through August 6, 2010. Summary of Nissan's Petition: Nissan states that the noncompliance is that the label identifying the amber air bag status telltale lamp for the front outboard passenger seating position is identified with the words ``PASSENGER AIR BAG'' instead of ``PASSENGER AIR BAG OFF.'' Nissan believes the noncompliance is inconsequential to motor vehicle safety for the following reasons: 1. The passenger air bag system on the subject vehicles operates as designed and automatically deactivates the passenger air bag when it is appropriate in accordance with the requirements in S19.2 of FMV55 No. 208. That is, the system requires no input from the operator to perform its intended function. Further, the front passenger airbag status telltale operates correctly and illuminates when the passenger air bag is deactivated as required by the standard. 2. The meaning of the air bag status telltale alone (without the identifying words) is unequivocal to the vehicle occupants. The telltale remains off when the passenger air bag is in the normal mode. When the passenger air bag is deactivated, the telltale is illuminated, showing an icon representing an air bag with an X drawn over it. This clearly represents a deactivated air bag. Nissan notes that in certain other markets, the telltale alone is deemed sufficient with no identifying words required next to the telltale. The identifying words ``passenger side air bag'' (without the word ``OFF'') do not confuse the otherwise clear and readily apparent meaning of the telltale. 3. Information provided in several locations in the vehicle owner's manual further reduces any possibility of operator confusion. If the meaning of telltale is unclear, the operator can refer to multiple explanations in the owner's manual. 4. Telltale Function is also described in Quick Reference Guide. 5. There have been no customer complaints, injuries, or accidents related to the word ``OFF'' missing from the label. Nissan has searched its databases and has found no cases of misunderstanding the telltale. 6. Nissan conducted an informal survey at Nissan's National Headquarters Building in Franklin, Tennessee. The building houses mostly business personnel (sales marketing, finance) and not design engineers that would have special understanding of the air bag systems. As employees were approaching the building to begin their workday, they were asked to participate in a survey regarding the Titan and that the survey would take about 30 seconds of their time. The participants represented a good cross-section of the general population by age, gender and race. The subject Titan pickup truck was equipped with the required yellow passenger side air bag status telltale that contained the ``no air bag'' symbol, but did not display the word ``OFF''. The passenger air bag telltale was illuminated. Survey participants were asked to describe the meaning of the telltale. Sixty people participated in the survey. Of the sixty people, 58 responded correctly that the telltale indicated the passenger side airbag was in suppressed mode. The survey shows that people understand the meaning of the passenger air bag telltale even with the word ``OFF'' missing. We note also that adding the word ``OFF'' did not help the two respondents to understand the meaning of the telltale. They would have needed to consult the Owner's Manual. Nissan acknowledges that this was an ad hoc survey that may not meet rigid statistical standards, nevertheless, we believe it is predictive of the results that would be obtained from a larger, controlled survey. 7. A decision to grant this petition would be consistent with arguably similar prior requests related to labeling issues. For example, NHTSA has previously granted petitions related to certain tire and tire placard labeling errors. Nissan also states that it has taken steps to correct the non- compliance in future production. Supported by the above stated reasons, Nissan believes that the described FMVSS No. 208 noncompliance is inconsequential to motor vehicle safety, and that its petition, to exempt it from providing recall notification of noncompliance as required by 49 U.S.C. 30118 and remedying the recall noncompliance as required by 49 U.S.C. 30120, should be granted. Discussion: Section S19.2.2 of FMVSS No. 208 specifically states:
Information Collection Available for Public Comments and Recommendations
Document Number: 2013-11427
Type: Notice
Date: 2013-05-14
Agency: Maritime Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, this notice announces the Maritime Administration's (MARAD's) intention to request extension of approval for three years of a currently approved information collection.
Information Collection Available for Public Comments and Recommendations
Document Number: 2013-11415
Type: Notice
Date: 2013-05-14
Agency: Maritime Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, this notice announces the Maritime Administration's (MARAD's) intention to request extension of approval for three years of a currently approved information collection.
Volkswagen Group of America, Incorporated, Grant of Petition for Decision of Inconsequential Noncompliance
Document Number: 2013-11412
Type: Notice
Date: 2013-05-14
Agency: National Highway Traffic Safety Administration, Department of Transportation
Volkswagen Group of America, Inc. (Volkswagen),\1\ has determined that certain model year (MY) 2011 Volkswagen Jetta passenger cars equipped with a TDI engine and Goodyear Eagle Vector 205/55 R16 94V XL tires, do not fully comply with paragraph S4.2.1.2 of Federal Motor Vehicle Safety Standard (FMVSS) No. 110, Tire selection and rims and motor home/recreation vehicle trailer load carrying capacity information for motor vehicles with a GVWR of 4,536 kilograms (10,000 pounds) or less. Volkswagen has filed an appropriate report pursuant to 49 CFR Part 573, Defect and Noncompliance Responsibility and Reports (dated June 7, 2011).
Grand Trunk Western Railroad Company-Acquisition of Operating Easement-CSX Transportation, Inc.
Document Number: 2013-11408
Type: Notice
Date: 2013-05-14
Agency: Surface Transportation Board, Department of Transportation
The Board is granting an exemption under 49 U.S.C. 10502 from the prior approval requirements at 49 U.S.C. 11323-25 for Grand Trunk Western Railroad Company (GTW), an indirect, wholly owned subsidiary of Canadian National Railway Company, to acquire from CSX Transportation, Inc. (CSXT) an exclusive, perpetual, non-assignable railroad operating easement over: 1. The location of the railroad at-grade crossing, at or near Leewood, between CSXT at milepost 00F Z 371.26 and Illinois Central Railroad Company (IC) at milepost 387.85, including the underlying right-of-way extending 50 feet on either side of the centerline of the CSXT tracks to IC's existing right-of-way and 75 feet on either side of the centerline of the IC tracks, together with appurtenances (other than the CSXT tracks outside the crossing) and related interlocking (Leewood Crossing); and 2. The location of the railroad at-grade crossing, at or near Aulon, between CSXT at milepost 0NI 224.05 and IC at milepost 390.0, including the underlying right-of-way extending approximately 50 feet on either side of the centerline of the CSXT track to IC's existing right-of-way and 50 feet on either side of the centerline of the IC tracks, together with appurtenances (other than the CSXT tracks outside the crossing) and related interlocking (Aulon Crossing). This acquisition is related to the Board's February 8, 2013 decision in this docket granting GTW's petition for exemption under 49 U.S.C. 10502 from the prior approval requirements at 49 U.S.C. 11323-25 to acquire from CSXT an operating easement over approximately 2.1 miles of CSXT's Memphis Terminal Subdivision between Leewood, Tenn., and Aulon, Tenn. After the Board served that decision, CSXT and GTW realized that they had unintentionally failed to seek authority permitting the operating easement to span the Aulon and Leewood Crossings. By a decision served on May 9, 2013, the Board is granting GTW's petition for supplemental authority and allowing it to expand its operating easement over these crossings.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2013-11382
Type: Proposed Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD was prompted by reports of excessive wear on the lower latch surface of the main landing gear (MLG) up-lock hook. This proposed AD would require revising the maintenance program. We are proposing this AD to detect and correct up-lock hooks worn beyond the wear limit, which could prevent the successful extension of the MLG using the primary landing gear extension system, which in combination with an alternate extension system failure could result in the inability to extend the MLG.
Airworthiness Directives; Airbus Airplanes
Document Number: 2013-11381
Type: Proposed Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede an existing airworthiness directive (AD) that applies to certain Airbus Model A318-111 and -112 airplanes, Model A319 series airplanes, Model A320 series airplanes, and Model A321 series airplanes. The existing AD currently requires repetitive inspections of the 80VU rack lower lateral fittings for damage; repetitive inspections of the 80VU rack lower central support for cracking; and corrective action if necessary. That existing AD also specifies optional terminating action for the repetitive inspections. Since we issued that AD, we have received reports of worn lower lateral fittings of the 80VU rack. This proposed AD would reduce the inspection compliance time, add an inspection of the upper fittings and shelves of the 80VU rack, and add airplanes to the applicability. We are proposing this AD to detect and correct damage or cracking of the 80VU fittings and supports, which could lead to possible disconnection of the cable harnesses to one or more computers and, if occurring during a critical phase of flight, could result in reduced control of the airplane.
Airworthiness Directives; Airbus Airplanes
Document Number: 2013-11380
Type: Proposed Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A300 series airplanes; Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). This proposed AD was prompted by a report that cracking was found in area 2 of the frame base fittings between frame 41 and frame 46. This proposed AD would require a check of maintenance records to determine if certain repairs were done in area 1 of the frame brace fittings, and, for affected airplanes, a detailed inspection for cracking in area 2 of the frame base fittings between frame 41 and frame 46, and repair if necessary. We are proposing this AD to detect and correct cracking in area 2 of the frame base fittings between frame 41 and frame 46, which could adversely affect the structural integrity of the airplane.
Notice of Final Federal Agency Actions on Proposed Highway in California
Document Number: 2013-11379
Type: Notice
Date: 2013-05-14
Agency: Federal Highway Administration, Department of Transportation
The FHWA, on behalf of Caltrans, is issuing this notice to announce actions taken by Caltrans, USACE and USFWS that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed State Route 41 Madera Passing Lanes project 0.3 miles north of Road 208 to 2.2 miles north of Road 208 in Madera County, in the State of California. Those actions grant licenses, permits, and approvals for the project.
Airworthiness Directives; Rolls-Royce plc Turbofan Engines
Document Number: 2013-11337
Type: Proposed Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We propose to supersede an existing airworthiness directive (AD) that applies to all Rolls-Royce plc (RR) model RB211 Trent 553-61, 553A2-61, 556-61, 556A2-61, 556B-61, 556B2-61, 560-61, and 560A2-61; and RB211 Trent 768-60, 772-60, and 772B-60; and RB211-Trent 875-17, 877-17, 884-17, 884B-17, 892-17, 892B-17, and 895-17; and RB211-524G2- T-19, -524G3-T-19, -524H-T-36, and -524H2-T-19 turbofan engines that have a high-pressure (HP) compressor stage 1 to 4 rotor disc installed, with a certain part number (P/N) installed. The existing AD requires repetitive inspections of the axial dovetail slots, and follow-on corrective action depending on findings. This proposed AD expands the population of affected parts. This proposed AD also changes, for the purposes of this AD, the definition of ``engine shop visit.'' We are proposing this AD to detect cracks in the HP compressor stage 1 and 2 disc posts, which could result in failure of the disc post and HP compressor blades, damage to the engine, and damage to the airplane.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2013-11327
Type: Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
This rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: 2013-11325
Type: Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
This rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Amendment of Class D Airspace; El Monte, CA
Document Number: 2013-11182
Type: Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class D airspace at El Monte Airport, El Monte, CA. This action, initiated by the FAA's biennial review of the El Monte Airspace area, creates additional Class D airspace to accommodate aircraft departures and arrivals. This improves the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2013-10659
Type: Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD was prompted by reports of two in-service incidents where the left main landing gear (MLG) failed to extend. This AD requires installing stopper plates on the aft uplock frames in the MLG bay adjacent to the right and left MLG uplock assemblies. We are issuing this AD to prevent incorrect installation of the upper bolt in the MLG uplock assembly, which could prevent the MLG from extending and could adversely affect the safe landing of the airplane.
Airworthiness Directives; the Boeing Company Airplanes
Document Number: 2013-10657
Type: Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-300, -400, and -500 series airplanes. This AD was prompted by reports of two in-service occurrences on Model 737-400 airplanes of total loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction feed capability on one engine, and in-flight shutdown of the engine. This AD requires repetitive operational tests of the engine fuel suction feed of the fuel system, and corrective actions if necessary. We are issuing this AD to detect and correct loss of the engine fuel suction feed capability of the fuel system, which, in the event of total loss of the fuel boost pumps, could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Twin Commander Aircraft LLC Airplanes
Document Number: 2013-10498
Type: Rule
Date: 2013-05-14
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Twin Commander Aircraft LLC Models 690, 690A, and 690B airplanes. This AD requires inspection for cracking of the outer fuselage attachments, the lower wing main spar, the vertical channels, the upper picture window channels, aft cabin pressure web, external wing to fuselage fillets, and fasteners; repair or replacement of damaged parts as necessary; and modification of the structure with reinforced parts. This AD was prompted by cracks found in the upper picture window frame channels, left- and right-hand wing main spar frame support channels, and aft pressure bulkhead web. This condition, if not corrected, could result in structural failure of the airplane. We are issuing this AD to correct the unsafe condition on these products.
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