Department of Transportation July 2008 – Federal Register Recent Federal Regulation Documents

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed 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:

As authorized by Public Law 105-383 and Public Law 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket MARAD-2008-0061, https:// www.regulations.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Public Law 105-383 and MARAD's regulations at 46 CFR part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.- flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR part 388.

In accordance with the Paperwork Reduction Act of 1995, this notice announces the Maritime Administration's (MARAD's) intention to request extension of approval (with modifications) for three years of a currently approved information collection.

We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to replace the cabin door rod ends with new parts including a redesigned non-binding hinge pin that replaces the existing pin at the upper door hinge. This AD results from two known occurrences of in-flight cabin door separation (one total separation and one retained by the door strut). The rod ends, a component of the door hinges, may fail and result in a door separation from the airplane while in flight. We are issuing this AD to prevent in-flight failure of the cabin door, which could result in door separation from the airplane.

We are adopting a new airworthiness directive (AD) for all Boeing Model 747 airplanes listed above. This AD requires repetitive inspections for broken or missing fasteners in the single-row hinge fasteners of the forward and aft cargo doors, and related investigative/corrective actions. This AD results from reports of broken and missing fasteners in the hinges of the forward and aft cargo doors in both the body hinge segments and the door hinge segments. We are issuing this AD to detect and correct broken or missing fasteners in the hinge segments with a single fastener row, which could lead to opening of the cargo door during flight and result in rapid decompression of the airplane.

The FAA is superseding an existing airworthiness directive (AD) for certain fuel injected reciprocating engines manufactured by Lycoming Engines. That AD currently requires inspection, and replacement if necessary, of externally mounted fuel injector fuel lines. This AD requires the same actions but adds additional engine models and clarifies certain compliance time wording. This AD also exempts engines that have a Maintenance and Overhaul Manual with an Airworthiness Limitations Section that requires inspection and replacement, if necessary, of externally mounted fuel injector lines. This AD results from Lycoming Engines revising their Mandatory Service Bulletin to add new engine models requiring inspection, and from the need to clarify a repetitive inspection compliance time. We are issuing this AD to prevent failure of the fuel injector fuel lines that would allow fuel to spray into the engine compartment, resulting in an engine fire.

We are adopting a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) helicopters. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority to identify and correct an unsafe condition on an aviation product. The Aviation Authority of Canada with whom we have a bilateral agreement states in the MCAI: ``Horizontal stabilizers part numbers 206-023-119-167 and 407-023-801-109 may have manufacturing flaws on the inside surface of the upper and/or lower skin at the tailboom attachment inserts. These flaws may result in cracking of the skin and failure of the horizontal stabilizer.'' The manufacturer's service information states that in addition to cracks, the horizontal stabilizer may have deformation or debonding around and between the inserts. We are issuing this AD to require actions to correct the unsafe condition on these products.

The FHWA is issuing this notice to advise the public that a First Tier Environmental Impact Statement (EIS) will be prepared for proposed improvements to I-70 from the end of the last ramp termini east of the Missouri and Kansas state line to east of the I-470 interchange, including the entire Kansas City Downtown Central Business District (CBD) Freeway Loop, in Jackson County, Missouri.

In accordance with National Environmental Policy Act (NEPA) regulations and FAA Order 1050.1E, Change 1, the FAA is announcing the availability of and requesting comments on the Draft EIS for the Spaceport America Commercial Launch Site, Sierra County, New Mexico. The Federal Aviation Administration (FAA), Office of Commercial Space Transportation is the lead Federal agency for the development of this EIS. Cooperating agencies include the Bureau of Land Management; the National Park Service; United States Department of the Army, White Sands Missile Range (WSMR); and the National Aeronautics and Space Administration. The Draft EIS was prepared in response to an application for a launch site operator license from the New Mexico Spaceport Authority (NMSA). Under the Proposed Action, the FAA would issue a launch site operator license to NMSA to operate a launch facility capable of accommodating both horizontal and vertical launches of suborbital launch vehicles (LVs). The vehicles may carry space flight participants, scientific experiments, or other payloads. The proposed site is located in Sierra County, approximately 30 miles southeast of Truth or Consequences, New Mexico, and 45 miles north of Las Cruces, New Mexico. The Draft EIS addresses the potential environmental impacts of issuing a launch site operator license for horizontal launches only (Alternative 1), vertical launches only (Alternative 2), and the No Action Alternative.

This action establishes Class D airspace at Albuquerque, NM. Establishment of an air traffic control tower at Double Eagle II Airport, Albuquerque, NM, has made this action necessary for the safety of Instrument Flight Rule (IFR) operations at the airport. This action also makes minor corrections to the geographic coordinates of the airport.

A direct final rule, published in the Federal Register April 14, 2008 (73 FR 19997) docket No. FAA-2008-0339, adding additional Class D and Class E airspace at Altus AFB, Altus, OK, is being withdrawn. Although the rule became effective June 5, 2008, charting of this airspace was never completed. A new rulemaking will be forthcoming with an effective date that coincides with the new charting date.

We are revising an earlier supplemental NPRM for the products listed above. This proposed 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:

Section 502 of title 23 of the United States Code directs the Secretary of Transportation (Secretary) to establish an Exploratory Advanced Research Program (EARP). The stated purpose of the EARP is to address longer-term and higher-risk research with potentially dramatic breakthroughs for improving the durability, efficiency, environmental impact, productivity and safety aspects of highway and intermodal transportation systems. The purpose of this notice is to announce exploratory advanced research that will take place under the EARP, to encourage interest in such work by organizations or individuals conducting related work or anticipating the results of such work, and to solicit comments about the long-term impact of such work on future research, technical innovation, or transportation industry practices.

We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed 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:

On October 25, 2002, the Federal Aviation Administration (FAA) published the final rule for Title 14, Code of Federal Regulations part 136, National Parks Air Tour Management (67 FR 65662). The rule became effective on January 23, 2003. On January 27, 2005, the FAA published a notice of opportunity for commercial air tour operators granted interim operating authority (IOA) under the National Parks Air Tour Management Act of 2000 (the Act) to review and self correct annual authorizations (70 FR 3972). The results were published by operator in the Federal Register on Thursday, June 23, 2005, (70 FR 36456). The comment due date was set for 70 FR 36456 and the IOA republished in the Federal Register on Friday, October 7, 2005 by park instead of by operator (70 FR 58778). This Notice is pursuant to the review and accepting of five (5) New Entrant applications and seeks public comment regarding this matter from interested parties.

This notice announces actions taken by the FHWA, USACE, and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project, the Interstate Routes 75 and 475 systems interchange, in the City of Toledo, Lucas County, in the State of Ohio. Those actions grant licenses, permits, and approvals for the project.

The FHWA is issuing this notice to advise the public that the Environmental Impact Statement (EIS) process for proposed highway improvements to Trunk Highway (TH) 169 in Crow Wing and Mille Lacs Counties, Minnesota is terminated. The original Notice of Intent for this EIS process was published in the Federal Register on July 17, 2000. A Revised Notice of Intent to revise the northern terminus was published in the Federal Register on February 4, 2002.

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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 certain Boeing Model 737-300 and -400 series airplanes. This AD requires testing and inspecting a certain web panel of the main wheel well pressure deck to determine the material type and thickness; and related investigative and corrective actions if necessary. This AD results from several reports indicating that cracks ranging from 0.8 to 8.0 inches long were found on a certain web panel of the main wheel well pressure deck. We are issuing this AD to prevent fatigue cracking in the web panel of the main wheel well pressure deck, which could result in venting and consequent decompression of the airplane.

We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires various repetitive inspections for cracking of the upper frame to side frame splice of the fuselage, and other specified and corrective actions if necessary. This AD also provides for an optional preventive modification, which terminates the repetitive inspections. This AD results from a report that the upper frame of the fuselage was severed between stringers S-13L and S-14L at station 747, and the adjacent frame at station 767 had a 1.3-inch-long crack at the same stringer location. We are issuing this AD to detect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could result in reduced structural integrity of the frame and adjacent lap joint. This reduced structural integrity can increase loading in the fuselage skin, which will accelerate skin crack growth and result in decompression 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:

PHMSA and the Federal Aviation Administration (FAA) are considering changes to requirements in the Hazardous Materials Regulations applicable to non-bulk packagings used to transport hazardous materials in air transportation. To enhance aviation safety, the two agencies are seeking to identify cost-effective solutions that can be implemented to reduce incident rates and potentially detrimental consequences without placing unnecessary burdens on the regulated community. We are soliciting comments on how to accomplish these goals, including measures to: (1) Enhance the effectiveness of performance testing for packagings used to transport hazardous materials on aircraft; (2) more clearly indicate the responsibilities of shippers that offer packages for air transport in the Hazardous Materials Regulations (HMR); and (3) authorize alternatives for enhancing package integrity. We are also considering ways to simplify current requirements. Commenters are also invited to present additional ideas for improving the safe transportation of hazardous materials by aircraft.

This document responds to two petitions for reconsideration of a final rule amending the Federal motor vehicle safety standard for power-operated window, partition, and roof panel systems. The subject final rule, statutorily mandated and published in April 2006, established a new safety requirement for vehicle power window switches, specifically that such switches have a ``pull-to-close'' design. That final rule set a compliance date of October 1, 2008, which was the same as the compliance date for a rule published in September 2004 that amended the standard to include a performance test to prevent inadvertent actuation of power window switches, particularly by children. Petitions for reconsideration were submitted by the Alliance of Automobile Manufacturers (Alliance) and DaimlerChrysler Corporation. The petitioners requested an extension of the compliance date by two years, as well as additional amendments to the standard. This document grants the requests common to both petitions for an additional two years to comply with the pull-to-close operability requirements of the April 2006 rule. It denies petitioners' other requests. Specifically, we are denying the request that power window switches be excluded from the ``pull-to-close'' design requirement if the power window systems are equipped with an automatic reversal feature. We are also denying a request for exclusion from the pull-to- close requirement for switches mounted in overhead locations and switches that operate vent-type power windows.

FMCSA announces receipt of applications from 19 individuals for exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations. If granted, the exemptions would enable these individuals to qualify as drivers of commercial motor vehicles (CMVs) in interstate commerce without meeting the Federal vision standard.