Department of Transportation March 2, 2015 – Federal Register Recent Federal Regulation Documents
Results 1 - 14 of 14
Ninety-Third Meeting: RTCA Special Committee 159, Global Positioning Systems (GPS)
The FAA is issuing this notice to advise the public of the ninety-third meeting of the RTCA Special Committee 159, Global Positioning Systems (GPS).
Revocation of Restricted Area R-2936, West Palm Beach, FL
This action removes restricted area R-2936, West Palm Beach, FL. The using agency informed the FAA they no longer have a requirement for this area; therefore, the airspace is being returned to the National Airspace System (NAS).
Amendment of Restricted Areas R-3801A, R-3801B, and R-3801C; Camp Claiborne, LA
This action updates using agency information for restricted areas R-3801A, R-3801B, and R-3801C, Camp Claiborne, LA. This is an administrative change to reflect an organizational transfer of using agency responsibilities within the United States Air Force. It does not affect the boundaries, designated altitudes, time of designation or activities conducted within the restricted areas.
Amendment of Restricted Area Boundary Descriptions; Cape Canaveral, FL
This action corrects a final rule; technical amendment, published in the Federal Register on December 15, 2014, that made minor adjustments to the boundary descriptions of restricted areas R-2932, R- 2933, R-2934 and R-2935 at Cape Canaveral, FL. Due to a submission error, one latitude/longitude point was omitted from the description of restricted area R-2935, Cape Canaveral, FL. This action corrects the boundary description of R-2935 by adding the missing point.
Notice and Request for Comments
As required by the Paperwork Reduction Act of 1995, 44 U.S.C. 3501-3519 (PRA), the Surface Transportation Board (STB or Board) gives notice of its intent to seek from the Office of Management and Budget (OMB) an extension of approval for the collection: Notifications of Trails Act Agreement and Substitute Sponsorship. Under 16 U.S.C. 1247(d) and its regulations, the STB will issue a Certificate of Interim Trail Use (CITU) or Notice of Interim Trail Use (NITU) to a prospective trail sponsor who offers to assume managerial, tax, and legal responsibility for a right-of-way that a rail carrier would otherwise abandon. The CITU/NITU permits parties, for 180 days, to negotiate for a railbanking agreement. If parties reach an agreement, the CITU/NITU automatically authorizes railbanking/interim trail use. If no agreement is reached, then upon expiration of the negotiation period, the CITU/NITU authorizes the railroad to exercise its option to fully abandon the line without further action by the Board. Pursuant to 49 CFR 1152.29, parties must jointly notify the Board when a trail use agreement has been reached, and must identify the exact location of the right-of-way subject to the agreement, including a map and milepost marker information. The rules also require parties to file a petition to modify or vacate the CITU/NITU if the trail use agreement applies to less of the right-of-way than covered by the CITU/ NITU. Finally, the rules require that a substitute trail sponsor must acknowledge that interim trail use is subject to restoration and reactivation at any time. Comments are requested concerning: (1) The accuracy of the Board's burden estimates; (2) ways to enhance the quality, utility, and clarity of the information collected; (3) 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; and (4) whether the collection of information is necessary for the proper performance of the functions of the Board, including whether the collection has practical utility. Submitted comments will be summarized and included in the Board's request for OMB approval. Description of Collection
Government/Industry Aeronautical Charting Forum Meeting
This notice announces the bi-annual meeting of the Federal Aviation Administration (FAA) Aeronautical Charting Forum (ACF) to discuss informational content and design of aeronautical charts and related products, as well as instrument flight procedures development policy and design criteria.
Federal Motor Vehicle Safety Standards; Seat Belt Assembly Anchorages
This document supplements NHTSA's March 2012 notice of proposed rulemaking (NPRM) to amend Federal Motor Vehicle Safety Standard (FMVSS) No. 210, ``Seat belt assembly anchorages,'' to specify a force application device (FAD) for use as a testing interface to transfer loads onto the seat belt anchorage system during compliance tests of anchorage strength. The agency received a number of comments on the NPRM that raised issues concerning the feasibility of the FAD proposal. After reviewing the comments, NHTSA has decided to propose in this SNPRM an alternative test procedure, i.e., one that would maintain the current FMVSS No. 210 body blocks and adopt procedures ensuring that the placement of the body blocks, at pre-load, is sufficiently specified. The agency requests comments on this alternative strategy and other potential enhancements to the current body block test procedure.
Petition for Exemption From the Federal Motor Vehicle Motor Theft Prevention Standard; General Motors Corporation
This document grants in full the General Motors Corporation's (GM) petition for an exemption of the Chevrolet Spark vehicle line in accordance with 49 CFR part 543, Exemption from Vehicle Theft Prevention Standard. This petition is granted because the agency has determined that the antitheft device to be placed on the line as standard equipment is likely to be as effective in reducing and deterring motor vehicle theft as compliance with the parts-marking requirements of 49 CFR part 541, Federal Motor Vehicle Theft Prevention Standard (Theft Prevention Standard).
Policy Regarding Datalink Communications Recording Requirements
This policy statement updates and clarifies how the FAA determines when datalink communications must be recorded as a function of the cockpit voice recorder operational regulations. This policy update eliminates unneeded limitations in current policy, and restates the FAA's intent that the requirement function as a performance-based regulation.
Ford Motor Company, Grant of Petition for Decision of Inconsequential Noncompliance
Ford Motor Company (Ford) has determined that certain model year (MY) 2010-2014 Transit Connect vehicles do not fully comply with paragraph S5.1 of Federal Motor Vehicle Safety Standard (FMVSS) No. 205, Glazing Materials. Ford has filed an appropriate report dated March 31, 2014, pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports.
General Motors, LLC; Ruling on Petition for Decision of Inconsequential Noncompliance
General Motors, LLC (GM) has determined that certain model year 2013 Chevrolet Malibu passenger cars manufactured between June 21, 2011 and July 24, 2012, do not fully comply with paragraphs S3.1.4.1 (a) and (b) of Federal Motor Vehicle Safety Standard (FMVSS) No. 102, Transmission Shift Position Sequence, Starter Interlock, and Transmission Braking Effect. GM has filed an appropriate report dated August 3, 2012, pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports.
Airworthiness Directives; Pratt & Whitney Turbofan Engines
We propose to adopt a new airworthiness directive (AD) for all Pratt & Whitney (PW) JT8D-217C and JT8D-219 turbofan engines. This proposed AD was prompted by reports of cracking in the low-pressure turbine (LPT) shaft. This proposed AD establishes a new lower life limit for these parts and would require removing affected LPT shafts from service using a drawdown plan. We are proposing this AD to prevent failure of the LPT shaft, which could lead to an uncontained engine failure and damage to the airplane.
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 2009-20-05 for certain Airbus Model A318, A319, A320, and A321 series airplanes. AD 2009-20-05 required one-time inspections for cracking, damage, correct installation, and correct adjustment of the main landing gear (MLG) door hinge and actuator fittings on the keel beam, and corrective actions if necessary. This new AD expands the applicability, reduces the compliance time, and requires repetitive inspections instead of the one-time inspection. This AD also requires revising the maintenance or inspection program. This AD was prompted by reports of cracks on fittings that had successfully passed certain required inspections. We are issuing this AD to detect and correct cracking on the MLG door hinge fitting and actuator fitting on the keel beam, which could lead to in-flight detachment of an MLG door, possibly resulting in injury to persons on the ground and/or damage to the airplane.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for certain Airbus Model A300 series airplanes, Model A300 B4-600, B4-600R, and F4- 600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). This AD was prompted by a report of chafing found on the overflow sensor harness of the surge tank, and subsequent contact between the electrical wiring and fuel tank structure. This AD requires a one-time inspection for chafing of the overflow sensor harness, and repair if necessary. This AD also requires modification of the sensor harness. We are issuing this AD to prevent chafing of the harness and subsequent contact between the electrical wiring and fuel tank structure, which could result in electrical arcing and a fuel tank explosion and consequent loss of the airplane.
This site is protected by reCAPTCHA and the Google
Privacy Policy and
Terms of Service apply.