Department of Transportation September 28, 2015 – Federal Register Recent Federal Regulation Documents

Notice of Final Federal Agency Actions on Proposed Highway in California
Document Number: 2015-24569
Type: Notice
Date: 2015-09-28
Agency: Federal Highway Administration, Department of Transportation
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, the United States (US) 101 Express Lanes Project from Post Miles 16.00 to 52.55 on US 101, and Post Miles 23.0 to 24.1 on State Route 85 in the County of Santa Clara, State of California. Those actions grant licenses, permits, and approvals for the project.
30-Day Notice of Application for New Information Collection Request OMB No. 2105-XXXX: Nondiscrimination on the Basis of Disability in Air Travel
Document Number: 2015-24562
Type: Notice
Date: 2015-09-28
Agency: Department of Transportation, Office of the Secretary
In accordance with the Paperwork Reduction Act of 1995 (44 U.S.C. chapter 35, as amended), this notice announces that the Department of Transportation's (DOT) Office of the Secretary (OST) is submitting a request to the Office of Management Budget (OMB) for approval of the new information collections described below. On November 12, 2013, the Department gave 60 day notice of its intent to obtain OMB control numbers authorizing the new information collections in its final rule amending the Air Carrier Access Act (ACAA) implementing regulation, 14 CFR part 382 (part 382), Nondiscrimination on the Basis of Disability in Air Travel. The purpose of this notice is to allow for an additional 30 days of public comment.
Amendment of Class E Airspace; Portland, OR
Document Number: 2015-24434
Type: Rule
Date: 2015-09-28
Agency: Federal Aviation Administration, Department of Transportation
This action modifies Class E surface area airspace designated as an extension to Class C airspace, and Class E airspace extending upward from 700 feet above the surface at Portland International Airport, Portland, OR. After reviewing the airspace, the FAA found the Portland VHF omnidirectional radio range/distance measuring equipment (VOR/DME) and Laker non-directional beacon (NDB) has been decommissioned, thereby necessitating airspace redesign for the safety and management of Instrument Flight Rules (IFR) operations at the airport. This action also corrects the geographic coordinates of the airport.
Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes
Document Number: 2015-24424
Type: Proposed Rule
Date: 2015-09-28
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Airbus Defense and Space S.A. (formerly known as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-235-200, and CN-235- 300 airplanes. This proposed AD was prompted by a report of cracks on the lugs of the inboard and outboard control rod fittings of the right hand (RH) and left hand (LH) side ailerons. This proposed AD would require a one-time non-destructive test (NDT) inspection of the inboard and outboard control rod fittings of the RH and LH side ailerons for cracks and corrosion, and repair if necessary. We are proposing this AD to detect and correct cracks and corrosion on the lugs of the inboard and outboard control rod fittings of the RH and LH side ailerons, which could lead to reduced controllability of the airplane.
Airworthiness Directives; Airbus Airplanes
Document Number: 2015-24423
Type: Proposed Rule
Date: 2015-09-28
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Airbus Model A318, A319, A320, and A321 series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) indicating that the fuselage skin repairs are subject to widespread fatigue damage (WFD). This proposed AD would require an inspection to determine whether any fuselage external skin (doubler) repairs have been accomplished, an inspection for cracking of certain repaired external fuselage skin areas in the fuselage, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking of the fuselage skin, which could result in reduced structural integrity of the airplane.
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