Department of Transportation February 7, 2018 – Federal Register Recent Federal Regulation Documents
Results 1 - 10 of 10
Agency Information Collection Activities: Extension of an Approved Information Collection Request; Comment Request; Generic Clearance for the Collection of Qualitative Feedback on Agency Service Delivery
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 its review and approval and invites public comment. The FMCSA requests approval to revise an existing ICR titled, ``Generic Clearance for the Collection of Qualitative Feedback on Agency Service Delivery,'' due to an increase in the annual cost to respondents. This ICR will allow for ongoing, collaborative and actionable communication between FMCSA and its customers and stakeholders. It will also allow feedback to contribute directly to the improvement of program management. On August 10, 2017, FMCSA published a Federal Register notice allowing for a 60-day comment period on this ICR. The agency received no comments in response to that notice.
Crash Preventability Demonstration Program
On July 27, 2017, FMCSA announced the initiation of a crash preventability demonstration program in which the Agency would accept requests for data review (RDRs) to evaluate the preventability of certain categories of crashes through its national data correction system known as DataQs. This notice provides additional information to help submitters and other interested parties understand the demonstration program.
Establishment of an Emergency Relief Docket for Calendar Year 2018
This Notice announces the establishment of FRA's emergency relief docket (ERD) for calendar year 2018. The designated ERD for calendar year 2018 is docket number FRA-2018-0013.
Nineteenth Tactical Operations Committee (TOC) Meeting
The FAA is issuing this notice to advise the public of a meeting of the Nineteenth TOC Meeting.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A321-211 and -231 airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by a determination that the flat-headed pin at the upper attachment point of the overhead stowage compartments at a certain frame may not sustain the maximum weight load for each flight phase. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-202, -203, -223, and -243 airplanes; and Model A340- 211, -212, -311, and -313 airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by a report of a hard contact that was found between the constant speed motor/generator feeder line route 6G/6E and the optional cabin temperature control pipe on the upper shell between certain frames. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 2005-19-28, which applied to certain Airbus Model A330-301, -321, -322, -341, and - 342 airplanes; and Model A340-200 and A340-300 series airplanes. AD 2005-19-28 required repetitive inspections for cracks in the aft face of the rear spar at the area adjacent to the bolt holes and the end of the build slot, and repair if necessary. AD 2005-19-28 also provided an optional terminating action for the repetitive inspections. This new AD was prompted by the results of a new fatigue and damage tolerance assessment, which determined that several compliance thresholds and intervals needed to be reduced. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 2015-02-18, which applied to all Airbus Model A330-201, -202, -203, -301, -302, and -303 airplanes. AD 2015-02-18 required a one-time ultrasonic inspection for fractures of all aft mount-pylon bolts of each engine. This new AD was prompted by the failure of a bolt on the aft engine mount upper beam, which was found to be caused by inappropriate in-production upper beam installation. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. We are issuing this AD to address the unsafe condition on these products.
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