Department of Transportation October 3, 2005 – Federal Register Recent Federal Regulation Documents

Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: 05-19746
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums 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, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
IFR Altitudes; Miscellaneous Amendments
Document Number: 05-19744
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.
Agency Information Collection Activity Under OMB Review, Request for Comments; Clearance of a New Information Collection Activity, Air Carriers Listing of Leading Outsource Maintenance Providers
Document Number: 05-19743
Type: Notice
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) approval for a new information collection. The FAA will use the data from the proposed collection to target those leading outsource maintenance providers that may have a higher risk level which in turn would merit an increase of FAA surveillance.
Modification of Class E Airspace; Wellington Municipal Airport, KS
Document Number: 05-19742
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
An examination of the controlled airspace for Wellington Municipal Airport, KS has revealed a discrepancy in the Airport Reference Point (ARP) and the size of the Class E airspace area. This action corrects the ARP and modifies the size of the Class E5 airspace area beginning at 700 feet above the surface. The radius of the airspace area is expanded from within a 6.3-mile radius to within a 6.4 mile radius of the airport. This action brings the Class E5 airspace area into compliance with FAA directives.
Modification of Class E Airspace; Sheldon Municipal Airport, IA
Document Number: 05-19741
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
This action modifies the size of the Class E5 airspace area beginning at 700 feet above the surface at Sheldon, IA to contain Instrument Flight Rule (IFR) operations in controlled airspace. The radius of the airspace area is expanded from within a 6.4-mile radius to within a 6.9-mile radius of the airport. This action brings the Class E5 airspace area into compliance with FAA directives.
Petition for Waiver of Compliance
Document Number: 05-19736
Type: Notice
Date: 2005-10-03
Agency: Federal Railroad Administration, Department of Transportation
Announcement of Establishment of the Federal Motor Carrier Safety Administration Medical Review Board; Request for Nominations
Document Number: 05-19726
Type: Notice
Date: 2005-10-03
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces the establishment of a Medical Review Board as requested by the recent passage of Safe, Accountable, Flexible, and Efficient Transportation Equity Act; A Legacy for Users (SAFETEA-LU). The Medical Review Board will provide scientific advice to The Secretary of Transportation and the Administrator of FMCSA on medical issues including the physical qualification requirements for commercial motor vehicle (CMV) operators. This announcement provides details about the purpose and functions of the FMCSA Medical Review Board, in accordance with the Federal Advisory Committee Act (FACA). This notice also discusses the Agency's medical research priorities and solicits applications from interested physicians to serve on the Medical Review Board. The Secretary of Transportation will appoint five physicians to the Medical Review Board, and the board will begin work in fiscal year 2006.
Aviation Proceedings, Agreements Filed the Week Ending September 9, 2005
Document Number: 05-19701
Type: Notice
Date: 2005-10-03
Agency: Department of Transportation, Office of the Secretary
Airworthiness Directives; Rolls-Royce Corporation (RRC) (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C28, -C28B, and -C28C Turboshaft Engines
Document Number: 05-19693
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) (RRC) Models 250-C28, - C28B, and -C28C turboshaft engines. This AD requires a onetime visual inspection of the seal joint in each passage between airfoils at the hub and shroud of third-stage turbine wheels, part number (P/N) 6899383. This AD results from reports of three failed third-stage turbine wheels and from the manufacturer's analysis of those failures. We are issuing this AD to prevent loss of power and uncommanded engine shutdown due to failure of the third-stage turbine wheel.
Michelin North America, Inc., Receipt of Petition for Decision of Inconsequential Noncompliance
Document Number: 05-19667
Type: Notice
Date: 2005-10-03
Agency: National Highway Traffic Safety Administration, Department of Transportation
Federal Motor Vehicle Safety Standards; Rearview Mirrors
Document Number: 05-19666
Type: Proposed Rule
Date: 2005-10-03
Agency: National Highway Traffic Safety Administration, Department of Transportation
In response to a petition for rulemaking submitted by Ms. Barbara Sanford, NHTSA published a Request for Comments (RFC) in the Federal Register on January 22, 2003 that included several questions regarding convex mirrors on commercial trucks. The Sanford petition asked the agency to amend our Federal Motor Vehicle Safety Standard (FMVSS) for rearview mirrors to require that all commercial trucks traveling on interstate highways have convex mirrors affixed to their front right and left fenders in order to provide drivers of these vehicles an increased field-of-view during lane change maneuvers, which the petitioner stated is necessary to eliminate a blind spot caused by the elevated position of commercial truck drivers relative to passenger cars. Prior to receiving the Sanford petition, the agency had decided to conduct research on heavy truck mirror systems, including fender- mounted mirrors. For reasons discussed in this document, the agency is withdrawing the RFC and is terminating this rulemaking, because additional research is necessary to assess the potential safety benefits of convex mirrors in this application.
Advisory Circular 33.4-3, Instructions for Continued Airworthiness; Aircraft Engine High Intensity Radiated Fields (HIRF) and Lightning Protection Features
Document Number: 05-19598
Type: Notice
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the issuance of Advisory Circular (AC) 33.4-3, Instructions for Continued Airworthiness; Aircraft Engine High Intensity Radiated Fields (HIRF) and Lightning Protection Features. This AC sets forth acceptable methods of compliance for aircraft engines with the provisions of Sec. 33.4, Instructions for Continued Airworthiness of Title 14 of the Code of Federal Regulations (14 CFR). This AC provides guidance for developing instructions for continued airworthiness to ensure the continued airworthiness of aircraft engine HIRF and Lightning protection features.
Gas Gathering Line Definition; Alternative Definition for Onshore Lines and Proposed Safety Standards
Document Number: 05-19455
Type: Proposed Rule
Date: 2005-10-03
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
On September 25, 1991, DOT published a notice of proposed rulemaking to revise the definition of ``gathering line'' in its gas pipeline safety standards. Because the proposal proved controversial, final action was postponed pending collection of additional information. In this Supplemental Notice of Proposed Rulemaking (SNPRM), PHMSA is proposing use of a consensus standard to distinguish onshore gathering lines. PHMSA's gas pipeline safety standards do not provide an adequate basis for distinguishing these pipelines from production facilities and transmission lines. In addition, PHMSA is proposing to establish safety standards for certain higher-risk onshore gathering lines, and to relax current standards on certain low-risk onshore gathering lines. (Onshore gathering lines in inlets of the Gulf of Mexico are not affected by this rulemaking.) Operators would use a new risk-based approach to determine which of its gathering lines are ``regulated onshore gathering lines'' and what safety standards the lines must meet. At present, PHMSA's safety standards do not apply to onshore gathering lines in rural locations, while onshore gathering lines in non-rural locations must meet the same requirements as transmission lines. This regulatory approach is insufficient to assure that conditions on gathering lines that pose a greater risk to the public and property are addressed. And it does not take into account the lower risk some other gathering lines pose. The intended effects of the proposed rules are improved identification of gathering lines, improved public confidence in the safety of gathering lines, and safety requirements better tailored to gathering line risks.
Airworthiness Directives; Various Transport Category Airplanes Manufactured by McDonnell Douglas
Document Number: 05-19438
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an existing airworthiness directive (AD) that applies to various transport category airplanes manufactured by McDonnell Douglas. We issued that AD to require a one-time test of the fire extinguishers for the engine and auxiliary power unit (APU), as applicable, to determine the capability of the Firex electrical circuits to fire discharge cartridges, and troubleshooting actions if necessary. This new AD removes certain transport category airplanes from the applicability of the existing AD. This AD results from reports indicating that fire extinguishers for the engine and auxiliary power unit had failed to discharge when commanded. We are issuing this AD to prevent failure of the fire extinguishers to fire discharge cartridges, which could result in the inability to put out a fire in an engine or in the APU.
Airworthiness Directives; Airbus Model A330-301, -321, -322, -341, and -342 Airplanes; and Model A340-200 and A340-300 Series Airplanes
Document Number: 05-19045
Type: Rule
Date: 2005-10-03
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A330-301, -321, -322, -341, and -342 airplanes; and Model A340-200 and A340-300 series airplanes. This AD requires 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. The AD also provides an optional terminating action for the repetitive inspections. This AD results from a report that, during fatigue tests of the wing, cracks were found in the vertical web of the rear spar between ribs 1 and 2 having initiated at the build slot. We are issuing this AD to detect and correct fatigue cracking in the vertical web of the wing rear spar, which could result in reduced structural integrity of the wing.
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.