Department of Transportation September 29, 2008 – Federal Register Recent Federal Regulation Documents

DOT proposes to modify a system of records under the Privacy Act of 1974. The system is FAA's Aviation Records on Individuals, which is being modified to reflect: (1) Eight new routine uses; (2) additions to the categories of records, (3) clarity to the purpose of the system, (4) changes to the titles of offices within the FAA. This system would not duplicate any other DOT system of records.

The FHWA invites public comments about our intention to request the Office of Management and Budget's (OMB) approval for a new information collection, which is summarized below under SUPPLEMENTARY INFORMATION. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.

This action revises the published description of three low altitude Alaskan compulsory reporting points, two high altitude reporting points, and revokes one high and low altitude reporting point in the vicinity of Bethel and Ketchikan. Specifically, the FAA is revising the description of CRACK, GARRS and MOCHA to address recent technical adjustments to their actual locations. Additionally, the FAA has determined that the FLUKE reporting point is no longer needed in the National Airspace System (NAS).

This action establishes Class D airspace at Victoria Regional Airport, Victoria, TX. Establishment of an air traffic control tower has made this action necessary for the safety of Instrument Flight Rule (IFR) operations at Victoria Regional Airport.

This action revises the Class E Airspace at Windsor Locks, Bradley International Airport, CT (BDL) to provide for adequate controlled airspace for those aircraft using Instrument Approach Procedures to the airport. The CHUPP NDB has been decommissioned, and after evaluation of the extension to the Windsor Locks Class C airspace defined using the CHUPP NDB, the FAA determined that the Class E3 airspace should be retained and extended 1 mile to provide adequate controlled airspace for the Instrument Approach Procedures to BDL. This action will enhance the safety and airspace management around the Bradley International Airport.

This action confirms the effective date of the direct final rule that establishes Class E5 airspace at Plains, TX, published in the Federal Register July 7, 2008, (73 FR 38313) Docket No. FAA-2008-0683.

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Fokker Model F.28 Mark 0070 and 0100 airplanes. That AD currently requires a one-time inspection of the main landing gear (MLG) main fitting for cracks, and repair if necessary. The existing AD also currently requires installing a placard and revising the airplane flight manual to include procedures to prohibit the application of brakes during backward movement of the airplane. This new AD requires repetitive eddy current inspections of the MLG main fitting and rework before further flight as applicable. This AD results from reports that a final solution eliminating the cause of the crack initiation mechanism is not yet available and that repetitive inspections are necessary. We are issuing this AD to detect and correct cracks in the MLG main fitting, which could result in reduced structural integrity of the MLG main fitting.

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

We are adopting a new airworthiness directive (AD) for all Lockheed Model 382, 382B, 382E, 382F, and 382G series airplanes. This AD requires revising the FAA-approved maintenance program by incorporating new airworthiness limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the accomplishment of certain fuel system modifications, the initial inspections of certain repetitive fuel system limitations to phase in those inspections, and repair if necessary. This AD results from a design review of the fuel tank systems. We are issuing this AD to prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: