Historic Preservation, Advisory Council August 20, 2015 – Federal Register Recent Federal Regulation Documents
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Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of Title 14, Code of Federal Regulations (14 CFR). The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of the FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.
Hours of Service of Drivers: CRST Expedited Inc., Application for Exemption
FMCSA announces that it has received an application from CRST Expedited, Inc. (CRST) for an exemption from certain provisions of the Agency's hours-of-service (HOS) regulations. CRST proposes that its team drivers be granted an exemption from the HOS rules pertaining to use of a sleeper berth (SB). Current HOS rules require that all SB rest regimens include, in part, the regular use of a SB period for at least 8 hourscombined with a separate period of at least 2 hours, either in the SB, off-duty or some combination of bothto gain the equivalent of at least 10 consecutive hours off duty. CRST proposes that its team drivers be allowed to take the equivalent of 10 consecutive hours off duty by splitting SB time into two periods totaling 10 hours, provided neither of the two periods is less than 3 hours. FMCSA requests public comment on CRST's application for exemption.
Hours of Service of Drivers; National Star Route Mail Contractors Association; Application for Exemption
FMCSA announces that it has received an application from the National Star Route Mail Contractors Association (NSRMCA) on behalf of its member motor carriers that transport mail under contract for the United States Postal Service (USPS). NSRMCA requests that its contract carriers be exempt from the ``14-hour rule'' of the Agency's hours-of- service regulations found in section 395.3(a)(2). NSRMCA specifically requests that a U.S. mail-carrying driver may elect to drive a U.S. mail-carrying commercial motor vehicle (CMV) no more than 10 hours following 8 consecutive hours off duty; and not drive after having been on duty 15 hours following 8 consecutive hours off duty. NSRMCA believes the exemption would positively impact safety, while reducing operating costs for USPS and contractors that provide Highway Contract Route services to the USPS. FMCSA requests public comment on the NSRMCA application for exemption.
Notice of Final Federal Agency Actions on Proposed Highway in California
The FHWA, on behalf of Caltrans, is issuing this notice to announce actions taken by Caltrans, that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project on northbound Interstate 680 from south of State Route (SR) 237 (Calaveras Boulevard) to north of SR 84 (Vallecitos Road) in or near the cities of Milpitas, Fremont, and Pleasanton, and the community of Sunol in Santa Clara and Alameda Counties in the State of California. Those actions grant licenses, permits, and approvals for the project.
Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems; Reopening of Comment Period
This action reopens the comment period for the regulatory evaluation associated with the FAA's June 11, 2013 Notice of Proposed Rulemaking (NPRM), Revisions to Operational Requirements for the Use of Enhanced Flight Vision Systems (EFVS) and to Pilot Compartment View Requirements for Vision Systems. The regulatory evaluation associated with the NPRM was not posted to the docket prior to the close of the comment period. Therefore, the FAA is reopening the comment period to allow the public the opportunity to adequately analyze the full regulatory evaluation for the NPRM. The FAA will accept comments on the regulatory evaluation only; and not on the regulatory changes proposed in the NPRM.
30-day Notice and Request for Comments: Continuation of Six Collections
As part of its continuing effort to reduce paperwork burdens, and as required by the Paperwork Reduction Act of 1995, 44 U.S.C. 3501- 3519 (PRA), the Surface Transportation Board (Board) gives notice that it is requesting from the Office of Management and Budget (OMB) approval without change of the six existing collections described below. The Board previously published a notice about this collection in the Federal Register on June 5, 2015, at 80 FR 32,201. That notice allowed for a 60-day public review and comment period. No comments were received. Comments may now be submitted to OMB concerning whether the particular collection of information is necessary for the proper performance of the functions of the Board, including whether the collection has practical utility; the accuracy of the Board's burden estimates; ways to enhance the quality, utility, and clarity of the information collected; and ways to minimize the burden of the collection of information on the respondents, including the use of automated collection techniques or other forms of information technology, when appropriate. Submitted comments will be included and/ or summarized in the Board's request for OMB approval.
Notice To Rescind Notice of Intent To Prepare Environmental Impact Statement, Interstate 64 Hampton Roads Bridge-Tunnel Corridor, Virginia
The Federal Highway Administration is issuing this notice to advise the public that FHWA is rescinding its Notice of Intent to prepare an Environmental Impact Statement for Interstate 64 Hampton Roads Bridge-Tunnel Corridor proposal in Virginia.
Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France) (Airbus Helicopters) Helicopters
We are superseding Airworthiness Directive (AD) 2013-21-01 for Eurocopter France Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2013-21-01 required certain inspections of each tail rotor pitch horn assembly (pitch horn) for a crack, replacing a cracked pitch horn before further flight, and a one-time visual inspection of pitch horns above certain hours time-in-service (TIS). This new AD retains the requirements of AD 2013-21-01 but requires a repetitive visual inspection for all pitch horns regardless of hours TIS. This AD was prompted by a report of a crack in the yoke of a pitch horn and is intended to detect a crack in the pitch horn to prevent failure of the pitch horn, loss of the anti-torque function, and subsequent loss of control of the helicopter.
Airworthiness Directives; Bell Helicopter Textron Canada (Bell) Helicopters
We are superseding Airworthiness Directive (AD) 2001-13-51 for Bell Model 206L-4, 407, and 427 helicopters. AD 2001-13-51 required inspecting certain driveshafts for a crack, a loose bolt or nut, or red powder residue and replacing a driveshaft if there is a crack, a loose bolt or nut, or red powder residue. AD 2001-13-51 also required notifying the FAA within 10 days if a crack is found in the driveshaft. This new AD retains the inspection requirement of AD 2001-13-51, expands the applicability to include the Model 429 helicopter, and removes the reporting requirement. This AD is intended to prevent failure of a driveshaft, loss of drive to the main rotor system, and a subsequent emergency landing.
Transportation for Individuals With Disabilities; Service Criteria for Complementary Paratransit Fares
This document seeks public comments on a petition for rulemaking from Access Services concerning the Department's regulations implementing the Americans with Disabilities Act (ADA) with respect to the method of determining the fare for a trip charged to an ADA paratransit eligible user. The petition asks the Department to revise its regulation to allow for a ``coordinated'' or two-tier fare structure. The current regulation provides that the fare shall not exceed twice the fare that would be charged to an individual paying full fare for a similar trip on the fixed route system.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A319, A320, and A321 series airplanes. This AD was prompted by reports that on airplanes equipped with sharklets, discretes (used to activate the load alleviation function) are connected on various flight computers using the same ground point. In these cases, the ground point segregation is no longer effective, and a single failure could lead to loss of sharklet identification by flight computers causing a return to the wing tip fence (no sharklet configuration) performance. This AD requires modification of the sharklet ground connection. We are issuing this AD to prevent loss of sharklet identification by the flight computers and subsequent reduced control of the airplane.
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 98-18-02 for certain Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model C4-605R variant F airplanes (collectively called A300-600 series airplanes). AD 98-18-02 required inspections to detect cracks in the center spar sealing angles adjacent to the pylon rear attachment and in the adjacent butt strap and skin panel, and correction of discrepancies. This new AD continues to require inspections for cracks. This new AD also requires a modification by cold expansion of the center spar sealing angles, replacement of both sealing angles and cold expansion of the attachment holes if necessary, and post-repair repetitive inspections and corrective actions if necessary. This AD was prompted by reports of cracking in the vertical web of the center spar sealing angles of the wing, and subsequent analyses that showed that the inspection threshold and interval specified in AD 98-18-02 must be reduced to allow timely detection of cracks on the sealing angles of the center spar, adjacent to rib 8. We are issuing this AD to prevent crack formation in the sealing angles, which could rupture the sealing angle and lead to subsequent crack formation in the bottom skin of the wing, and result in reduced structural integrity of the center spar section of the wing.
Airworthiness Directives; Bombardier, Inc. Airplanes
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes. This AD was prompted by reports of a disconnect between the elevator lever and control rod. This AD requires replacement of left and right fixed control rods and lever assemblies of the elevator control system. We are issuing this AD to prevent a disconnect between the elevator lever and control rod, which could lead to un-commanded elevator movement of the associated control surface, a large difference between the position of the left and the right elevator control surfaces, and consequent reduced controllability of the airplane and degradation of the structural integrity of the horizontal stabilizer.
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