Historic Preservation, Advisory Council August 2015 – Federal Register Recent Federal Regulation Documents

We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777-200 series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) indicating that the skin lap splices at certain stringers in certain fuselage sections are subject to widespread fatigue damage (WFD). This proposed AD would require inspections to detect cracking of fuselage skin lap splices in certain fuselage sections, and corrective actions if necessary; modification of left-side and right-side lap splices; and post-modification repetitive inspections for cracks in the modified lap splices, and corrective actions if necessary. We are proposing this AD to detect and correct fatigue cracking of the skin lap splices, and consequent risk of sudden decompression and the inability to sustain limit flight and pressure loads.

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company Model 500, 501, 550, 551, S550, 560, and 650 airplanes. This AD was prompted by reports of smoke and/or fire in the tailcone caused by sparking due to excessive wear of the brushes in the air conditioning (A/C) motor. This AD requires inspections to determine if certain A/C compressor motors are installed and to determine the accumulated hours on certain A/C compressor motor assemblies; and repetitive replacement of the brushes in the A/C compressor motor assembly, or, as an option to the brush replacement, deactivation of the A/C system and placard installation; and return of replaced brushes to Cessna. We are issuing this AD to prevent the brushes in the A/C motor from wearing down beyond their limits, which could result in the rivet in the brush contacting the commutator, causing sparks and consequent fire and/or smoke in the tailcone with no means to detect or extinguish the fire and/or smoke.

We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. This AD requires inspecting the swashplate assembly rotating star to determine whether a ferrule was installed. If a ferrule exists, this AD requires inspecting the rotating star for a crack and removing any cracked rotating star. This AD was prompted by a report that reconditioning the rotating swashplate per a certain repair procedure could result in the rotating star cracking. The actions of this AD are intended to detect a crack in the rotating star and prevent failure of the rotating star and subsequent loss of control of the helicopter.

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by an in-service report of an uncommanded and unannunciated nose wheel steering during airplane pushback from the gate. This AD requires installing new cable assemblies with a pull-down resistor. We are issuing this AD to prevent an uncommanded nose wheel steering during takeoff or landing in the event of an open circuit in the steering system, and possible consequent runway excursion.

We are superseding Airworthiness Directive (AD) 2011-08-51 for certain The Boeing Company Model 737-300, -400, and -500 series airplanes. AD 2011-08-51 required repetitive inspections of the lap joint at certain stringers along the entire length from certain body stations. This new AD expands the inspection area, requires additional inspections for cracks and open pockets, requires corrective actions if necessary, and revises the compliance times. This AD was prompted by an evaluation by the design approval holder (DAH) that has determined that the lower fastener holes in the lower skin of the fuselage lap splice are subject to widespread fatigue damage (WFD). We are issuing this AD to detect and correct fatigue cracking of the lower fastener holes in the lower skin of the fuselage lap splice, which could result in reduced structural integrity of the airplane.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 29, 2015. The respondents to this information collection are FAR part 135 and part 121 operators seeking airman certification and approval of aircraft dispatcher courses. The FAA uses the information to ensure compliance and adherence to the regulations.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 29, 2015. Regulation generates a need for new designated pilot examiners and designated airworthiness representatives to support the certification of new light-sport aircraft, pilots, flight instructors, and ground instructors.

This action establishes Class D airspace, Class E surface area airspace, and Class E airspace extending upward from 700 feet above the surface at Aurora State Airport, Aurora, OR, to accommodate standard instrument approach procedures for the new air traffic control tower. This action enhances the safety and management of Instrument Flight Rules (IFR) operations at the airport.

In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR part 107, subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. Each mode of transportation for which a particular special permit is requested is indicated by a number in the ``Nature of Application'' portion of the table below as follows: 1Motor vehicle, 2Rail freight, 3Cargo vessel, 4Cargo aircraft only, 5Passenger-carrying aircraft.

This action proposes special conditions for the Cirrus Aircraft Corporation Model SF50 airplane. This airplane will have a novel or unusual design feature(s) associated with installation of an Auto Throttle System. 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.

FMCSA announces its decision to renew the exemptions from the Epilepsy and Seizure Disorders requirement in the Federal Motor Carrier Safety Regulations for 29 individuals. FMCSA has statutory authority to exempt individuals from the Epilepsy and Seizure Disorders 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.

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 review and approval and invites public comment. The FMCSA requests approval to revise an ICR entitled, ``Motor Carrier Identification Report,'' which is used to identify FMCSA regulated entities, help prioritize the agency's activities, aid in assessing the safety outcomes of those activities, and for statistical purposes. This ICR is being revised due to a Final Rule titled, ``Unified Registration System,'' (78 FR 52608) dated August 23, 2013 which will require regulated entities to file for registration via a new online Form MCSA-1 and eliminate the Forms MCS- 150B and MCS-150C contained in the ICR. The Form MCS-150 will be retained for use by the small number of Mexico-domiciled motor carriers that seek authority to operate beyond the United States municipalities on the United States-Mexico border and their commercial zones because they are not included within the scope of the Unified Registration Final Rule.

The Federal Transit Administration (FTA) received a Buy America waiver request from the Colorado Department of Transportation on behalf of the Town of Mountain Village for replacement parts for a gondola rehabilitation project. A non-availability waiver is needed because Mountain Village intends to rehabilitate the gondola system with FTA funding and the replacement parts do not comply with Buy America requirements. In accordance with 49 U.S.C. 5323(j)(3)(A), FTA published a notice of the waiver request and sought public comment in deciding whether to grant the request. Having received no comments opposing the waiver, FTA is hereby granting a non-availability waiver for the replacement gondola components to be procured by Mountain Village for the gondola refurbishment projects described herein.

We propose to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 900EX airplanes and FALCON 2000EX airplanes. This proposed AD was prompted by a report of significant fuel leakage at the middle position of the left outboard slat. This proposed AD would require modifying the assembly of the slat extension mechanical stop. We are proposing this AD to prevent failure of the assembly of the slat extension mechanical stop, which if not corrected, could lead to a significant fuel leak and result in an uncontained fire.

This rule amends, suspends, or removes 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 for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

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.

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.

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.

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.

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.

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.