Department of Transportation February 4, 2005 – Federal Register Recent Federal Regulation Documents
Results 1 - 3 of 3
Hours of Service of Drivers
On January 24, 2005, the Federal Motor Carrier Safety Administration (FMCSA) published in the Federal Register (70 FR 3339) a Notice of Proposed Rulemaking (NPRM) regarding hours of service of commercial motor vehicle drivers. In that NPRM, FMCSA announced it is reviewing and reconsidering the regulations on hours of service of drivers published on April 28, 2003, and amended on September 30, 2003. In the docket to this January 24, 2005, NPRM, FMCSA re-filed the same Regulatory Impact Analysis (RIA), or comprehensive analysis of economic benefits and costs of the proposed rule, as was filed in the docket for the April 2003 final rule. However, effective January 1, 2005, the Office of Management and Budget (OMB) imposed new analytical requirements on Federal agencies regarding the preparation of RIAs for economically significant rulemakings. These new requirements include an uncertainty analysis, or an analysis of the ``degree of uncertainty'' associated with key variables used in the analysis (i.e., the percent of all truck-related crashes where commercial driver fatigue is a factor) and how significantly that uncertainty affects the benefit and cost estimates derived. A primary value of uncertainty analysis is its ability to highlight those key variables where additional data collection (to reduce uncertainty) would most benefit the decision making process. Additionally, OMB now requires a cost-effectiveness analysis for those rulemakings where improved public health and safety are the primary benefits. The cost effectiveness of a regulatory action is typically measured as a ratio of the change in costs occasioned by the action compared to its positive results (i.e., lives saved). A primary value of cost-effectiveness analysis is its ability to identify regulatory options that achieve the most effective use of the resources available without requiring monetization of all of the relevant benefits or costs. In light of these new requirements, FMCSA has prepared an addendum to the original RIA containing the two supplemental analyses and has made it available in Docket FMCSA-2004- 19608.
Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes
The FAA is revising an existing airworthiness directive (AD), which applies to certain McDonnell Douglas Model MD-90-30 airplanes. This AD requires a one-time general visual inspection to detect wire chafing damage and to determine adequate clearance between the disconnect panel structure and the wires above the aft left lavatory; and corrective actions, if necessary. This new AD revises the applicability of the existing AD. This AD is prompted by the determination that certain airplanes unaffected by the existing AD are subject to the unsafe condition, and certain other airplanes should be removed from the applicability. We are issuing this AD to prevent damage to certain wires due to contact between the wires and the adjacent structure, which could result in electrical arcing and consequent smoke and fire in the cabin.
Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to all Boeing Model 767-200, -300, and -300F series airplanes. That AD currently requires examination of maintenance records to determine if Titanine JC5A (also known as Desoto 823E508) corrosion inhibiting compound (``C.I.C.'') was ever used; inspection for cracks or corrosion and corrective action, if applicable; repetitive inspections and C.I.C. applications; and modification of the aft trunnion area of the outer cylinder, which terminates the need for the repetitive inspections and C.I.C. applications. This new AD also requires, for certain other airplanes, repetitive inspections for cracks or corrosion, corrective action if necessary, and repetitive C.I.C. applications. This AD is prompted by a report that JC5A was used on more airplanes during production than previously identified. We are issuing this AD to prevent severe corrosion in the main landing gear (MLG) outer cylinder at the aft trunnion, which could develop into stress corrosion cracking and consequent collapse of the MLG.
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