Department of Transportation September 26, 2007 – Federal Register Recent Federal Regulation Documents

This document proposes to increase the maximum aggregate civil penalties for violations of the odometer tampering and disclosure requirements and certain administrative provisions of the Energy Policy and Conservation Act. This action would be taken pursuant to the Federal Civil Monetary Penalty Inflation Adjustment Act of 1990, as amended by the Debt Collection Improvement Act of 1996, which requires us to review and, as warranted, adjust penalties based on inflation at least every four years.

In accordance with the Paperwork Reduction Act of 1995, FMCSA announces its plan to submit the Information Collection Request (ICR) described below to the Office of Management and Budget (OMB) for review and approval. The ICR is titled, ``Training Certification for Drivers of Longer Combination Vehicles (LCVs).'' This ICR is necessary because the training certificate serves as proof that a driver has successfully completed the training required before he or she may operate an LCV on the Nation's highways. The hiring motor carrier is required to maintain a copy of the training certificate in the LCV driver's qualification file. The document is subject to review by Federal or State enforcement officials. On June 28, 2007, FMCSA published a Federal Register notice allowing for a 60-day comment period on the ICR. One comment was received.

The FAA issues these special conditions for the Boeing Model 787-8 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These novel or unusual design features are associated with carbon fiber reinforced plastic used in the construction of the fuselage. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards for impact response characteristics to ensure survivable crashworthiness. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing standards. We will issue additional special conditions for other novel or unusual design features of the Boeing Model 787-8 airplanes.

Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), and 5 U.S.C. 552b(c), notice is hereby given of a telephone conference for the Reusable Launch Vehicle Working Group (RLVWG) of the Commercial Space Transportation Advisory Committee (COMSTAC). The main issue for discussion will be the formation of a group within the RLVWG to examine training standards for crew and space flight participants. The telephone conference will take place on Friday, October 5, 2007 starting at 9:30 Eastern Daylight Time. For the call-in telephone number and the passcode, contact the Contact Person listed below.

In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501, et seq.), this notice announces that the Information Collection Requirement (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for review and comment. The ICR describes the nature of the information collection and its expected burden. The Federal Register notice with a 60-day comment period soliciting comments on the following collection of information was published on July 20, 2007 (See 72 FR 39886).

The FAA is adopting a new airworthiness directive (AD) for all Viking Air Limited Model DHC-7 airplanes. This AD requires an inspection of certain SM-200 servo drive units (power servo motor and housing assemblies) for certain markings, related investigative action if necessary, and modification if necessary. This AD results from a report that some SM-200 servo drive units that were not in configuration MOD H are installed on Model DHC-7 airplanes. MOD H prevents the internal clutch fasteners from backing out. We are issuing this AD to prevent the possibility of internal clutch fasteners from backing out, which could cause an inadvertent servo engagement and consequent reduced controllability of the airplane.

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100B SUD, 747-200B, 747-200C, 747-200F, 747- 300, 747-400, 747-400D, 747-400F, and 747SP series airplanes. This AD requires reconfiguring the clamps of certain wire bundles and applying insulating sealant to certain fasteners inside the fuel tanks. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent arcing inside the fuel tanks in the event of a lightning strike or high-powered short circuit, which could result in a fuel tank explosion or fire.

The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 186 Automatic Dependent Surveillance- Broadcast (ADS-B).