Department of Transportation March 30, 2012 – Federal Register Recent Federal Regulation Documents
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High Density Traffic Airports; Notice of Determination Regarding Low Demand Periods at Ronald Reagan Washington National Airport
This action announces an FAA determination that 10 p.m. to 10:59 p.m. no longer is a low demand period at Ronald Reagan Washington National Airport (DCA). As a result of this determination, the FAA will allocate available slots in that period on a temporary basis subject to recall, and the FAA may conduct a lottery in the future to allocate available slots in that period.
Notice of Public Availability of the final Environmental Assessment (EA) and Finding of No Significant Impact/Record of Decision (FONSI/ROD) Signed March 20, 2012, for the Evaluation of the Potential Environmental Impacts Associated With the Dual Track Airport Project for the Brookings Regional Airport in Brookings, SD
The FAA has issued the final EA and FONSI/ROD for the Dual Track Airport Project for Brookings Regional Airport. The EA was prepared in accordance with the National Environmental Policy Act (NEPA) of 1969, as amended, FAA Orders 1050.1E, ``Environmental Impacts: Policies and Procedures'' and FAA Order 5050.4B, ``NEPA Implementing Instructions for Airport Actions''.
Deadline for Notification of Intent To Use the Airport Improvement Program (AIP) Primary, Cargo, and Nonprimary Entitlement Funds for Fiscal Year 2012
The Federal Aviation Administration (FAA) announces May 1, 2012, as the deadline for each airport sponsor to notify the FAA whether or not it will use its fiscal year 2012 entitlement funds available under Section 47105(f) of Title 49, United States Code, to accomplish Airport Improvement Program (AIP)-eligible projects that the sponsor previously identified through the Airports Capital Improvement Plan (ACIP) process during the preceding year. This notice must address all entitlement funds apportioned for fiscal year 2012. After Friday, August 10, 2012, the FAA will carry over all remaining entitlement funds, and the funds will not be available again until at least the beginning of fiscal year 2013. This notification requirement does not apply to non- primary airports covered by the block-grant program.
Special Conditions: Airbus, A350-900 Series Airplane; Crew Rest Compartments
This action proposes special conditions for Airbus A350-900 series airplanes. These airplanes will have novel or unusual design features associated with two separate Crew Rest Compartments: a Flight Crew Rest Compartment (FCRC) intended to be occupied by flight crew members only, and a Cabin Crew Rest Compartment (CCRC) intended to be occupied by cabin crew members. Both types of Crew Rest Compartments (CRC) are installed in the overhead area with access from the main deck. 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.
Buy America Waiver Notification
This notice provides information regarding the FHWA's finding that a partial Buy America waiver is appropriate for the obligation of Federal-aid Congestion Mitigation and Air Quality (CMAQ) improvement program funds for the purchase of eight 2012 Ford Escape hybrid four- wheel drive vehicles by Merced County, CA.
Pipeline Safety: Public Comment on Leak and Valve Studies Mandated by the Pipeline Safety, Regulatory Certainty, and Job Creation Act of 2011
The Department of Transportation (DOT), Pipeline and Hazardous Materials Safety Administration (PHMSA) is providing an important opportunity through this notice for all stakeholders to publically comment on the scope of recently commissioned studies involving leak detection systems and valves. This action and others described within this notice will support the comprehensive investigation of topics and issues Congress has charged to PHMSA.
Notice of Schedule Information Submission Deadline for O'Hare International Airport, San Francisco International Airport, John F. Kennedy International Airport, and Newark Liberty International Airport for the Winter 2012-2013 Scheduling Season
Under this notice, the FAA announces the submission deadline of May 10, 2012, for Winter 2012-2013 flight schedules at Chicago's O'Hare International Airport (ORD), San Francisco International Airport (SFO), New York's John F. Kennedy International Airport (JFK), and Newark Liberty International Airport (EWR) in accordance with the International Air Transport Association (IATA) Worldwide Slot Guidelines. The deadline coincides with the schedule submission deadline for the IATA Slot Conference for the Winter 2012-2013 scheduling season.
Federal Motor Vehicle Safety Standards; Bus Emergency Exits and Window Retention and Release
In this final rule, which was preceded by a notice of proposed rulemaking, NHTSA is making several housekeeping amendments to the Federal motor vehicle safety standard for bus emergency exits. First, based on a proposal made in response to a petition for rulemaking from the School Bus Manufacturers Technical Council (SBMTC), NHTSA amends the standard to specify that the exterior release (the exterior handle) for school bus rear emergency exit doors may be located opposite the door hinges, rather than located in the middle of the door. Second, this final rule also clarifies the standard as to the number of force applications that are required to open a window or roof emergency exit. Third, in response to a comment on the proposed rule, this document makes a technical correction by removing a reference to a no-longer existent figure. These amendments correct or clarify the requirements of the standard. We believe most, if not all, school buses are currently designed to meet the corrected or clarified requirements.
Federal Motor Vehicle Safety Standards; Seat Belt Assembly Anchorages; Incorporation by Reference
This NPRM proposes to amend Federal Motor Vehicle Safety Standard No. 210, ``Seat belt assembly anchorages,'' to specify a new force application device for use as a testing interface to transfer loads onto the seat belt anchorage system during compliance tests of anchorage strength. The device represents a human torso and pelvis. The new device comes in two sizes, one representative of a mid-size adult male, and the other of a small occupant. We propose both sizes be used in FMVSS No. 210. We believe that the devices provide a consistent test configuration and load path to the seat belt assembly anchorages. We are proposing this amendment because the devices are significantly easier to use than the current body blocks.
Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO) TSO-C69b and Installed on Airbus Airplanes
We are superseding an existing airworthiness directive (AD) for Goodrich Evacuation Systems approved under TSO TSO-C69b and installed on Model A330-200 and -300 series airplanes, Model A340-200 and -300 series airplanes, and Model A340-500 and -600 series airplanes. That AD currently requires inspecting to determine the part number of the pressure relief valves on the affected Goodrich evacuation systems, and corrective action if necessary. This new AD requires inspecting to determine the part number of the pressure relief valves on the affected Goodrich evacuation systems and replacing certain pressure relief valves, and adds airplanes to the applicability. This AD was prompted by reports that during workshop testing, certain pressure relief valves, which were required by the existing AD, did not seal and allowed the pressure in certain slides/ rafts to fall below the minimum raft mode pressure for the unit. We are issuing this AD to prevent loss of pressure in the escape slides/rafts after an emergency evacuation, which could result in inadequate buoyancy to support the raft's passenger capacity during ditching and increase the chance for injury to raft passengers.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for all Airbus Model A340-500 and Model -600 series airplanes. This AD requires performing repetitive high frequency eddy current inspections of the external radius on upper horizontal cruciform fitting at frame (FR) 47 on the left- and right-hand sides for cracks, and repairing the cracks if necessary. This AD was prompted by reports that during fatigue testing, damages occurred in the external radius on the upper horizontal cruciform fitting at FR47 on the left- and right-hand sides. We are issuing this AD to detect and correct fatigue cracking, which could adversely affect the structural integrity of the airplane.
Airworthiness Directives; DASSAULT AVIATION Airplanes
We are adopting a new airworthiness directive (AD) for all DASSAULT AVIATION Model MYSTERE-FALCON 900 airplanes. This AD was prompted by multiple reports of fuel leakage from a defective fuel high-level sensor located in the wing front spar. This AD requires inspecting to determine fuel quantity sensors part numbers and replacing of certain fuel quantity sensors with new fuel quantity sensors. We are issuing this AD to prevent internal fuel leakage with significant fuel vapors, which could result in a fire hazard.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-200, A330-300, A340-500, and A340-600 series airplanes. This AD requires a detailed inspection for cracked and missing nuts, and replacement of cracked or missing nuts with new nuts having the same part number. This AD was prompted by reports of cracked nuts detected during production. We are issuing this AD to detect and correct cracked or missing nuts, and replace all affected nuts in multiple locations (including fuel tank areas) that could result in reduced structural integrity of the airplane.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A321-131, -211, -212, and -231 airplanes. This AD requires a rotating probe inspection for cracking of the lower panel bore holes of the center wing box (CWB), and corrective actions if necessary. This AD was prompted by reports of incorrect installation of rib pads of the lower aft panel of the CWB due to poor clamping during drilling, and reports that metal chips trapped between panels and stiffeners could impact the fatigue life of CWB panels. We are issuing this AD to detect and correct cracking and damage in the bore holes of the rib pads of the lower forward and aft panels of the CWB which could result in reduced structural integrity of the wings.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for all Airbus Model A340-600 series airplanes. This AD requires a detailed inspection for abnormalities of the ball lock retainer on the off-wing ramp slides; for closure of the soft cover; for full engagement of the slide release pin; for broken, missing, and improper placement of the safety tie thread on the slide release pin; and for proper functioning of the vent valve; and replacement of the off-wing ramp slides if necessary. This AD was prompted by reports of in-flight loss of the blow-out panel and the slide unit from a right-hand off-wing ramp- slide. We are issuing this AD to detect and correct abnormalities of the ball lock retainer, if the soft cover is open, if the slide pin release is not engaged or the safety tie thread is missing, broken, or improperly placed and the vent valve is not functioning properly, which could result in in-flight loss of the off-wing ramp slide.
Airworthiness Directives; DG Flugzeugbau GmbH Gliders
We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Models DG-500 Elan Orion, DG-500 Elan Trainer, DG-500/ 20 Elan, DG-500/22 Elan, DG-500M, and DG-500MB gliders. 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 damage to the bulkhead of the glider's center of gravity (CG) tow hook that, if not detected and corrected, may lead to failure of the fiberglass structure during a winch launch. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
We are adopting a new airworthiness directive (AD) for Pilatus Aircraft Ltd. Models PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC- 6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2- H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 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 loose elevator and rudder hinge bolts caused by incorrect torquing and locking of the bolts, which could lead to in-flight failure of the elevator or rudder attachment. We are issuing this AD to require actions to address the unsafe condition on these products.
Establishment of Class E Airspace; Marion, AL
This action establishes Class E Airspace at Marion, AL, to accommodate the new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures serving Vaiden Field. This action enhances the safety and airspace management of Instrument Flight Rules (IFR) operations within the National Airspace System.
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