Department of Transportation May 5, 2009 – Federal Register Recent Federal Regulation Documents

Motor Carrier Safety Advisory Committee Public Meeting
Document Number: E9-10340
Type: Notice
Date: 2009-05-05
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces that the Motor Carrier Safety Advisory Committee (MCSAC) will hold a committee meeting. The meeting is open to the public.
Qualification of Drivers; Exemption Renewals; Vision
Document Number: E9-10339
Type: Notice
Date: 2009-05-05
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA previously announced its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 23 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemptions will provide a level of safety that will be equivalent to, or greater than, the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Regulations Governing Fees for Services Performed in Connection With Licensing and Related Services-2009 Update
Document Number: E9-10304
Type: Rule
Date: 2009-05-05
Agency: Surface Transportation Board, Department of Transportation
The Board adopts its 2009 User-Fee Update and revises its fee schedule to reflect increased costs associated with the January 2009 government salary increases, changes to the Board's overhead costs, and to also reflect changes in the government fringe benefits.
Airworthiness Directives; Boeing 737-600, -700, -700C, and -800 Series Airplanes
Document Number: E9-10303
Type: Proposed Rule
Date: 2009-05-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, and -800 series airplanes. This proposed AD would require repetitive lubrications of the right and left main landing gear (MLG) forward trunnion pins. This proposed AD also would require an inspection for discrepancies of the transition radius of the MLG forward trunnion pins, and corrective actions if necessary. For certain airplanes, this proposed AD would also require repetitive detailed inspections for discrepancies (including finish damage, corrosion, pitting, and base metal scratches) of the transition radius of the left and right MLG trunnion pins, and corrective action if necessary. Replacing or overhauling the trunnion pins would terminate the actions required by this AD. This proposed AD results from a report that the protective finishes on the forward trunnion pins for the left and right MLG might have been damaged during final assembly. We are proposing this AD to prevent stress corrosion cracking of the forward trunnion pins, which could result in fracture of the pins and consequent collapse of the MLG.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes
Document Number: E9-10302
Type: Proposed Rule
Date: 2009-05-05
Agency: Federal Aviation Administration, Department of Transportation
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:
Norfolk Southern Railway Company-Abandonment Exemption-in Floyd and Polk Counties, GA
Document Number: E9-10258
Type: Notice
Date: 2009-05-05
Agency: Surface Transportation Board, Department of Transportation
Commercial Driver's License (CDL) Standards; Rotel North American Tours, LLC; Amendment of Exemption
Document Number: E9-10209
Type: Notice
Date: 2009-05-05
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces that the Rotel North American Tours, LLC (Rotel), has applied for amendment of its existing exemption that permits 22 named drivers, employed by Rotel and possessing German CDLs, to operate commercial motor vehicles (CMVs) in the U.S. without a CDL issued by one of the States. Rotel proposes to amend the roster of 22 exempt Rotel drivers in order to substitute three new Rotel drivers for three drivers no longer employed by Rotel. The new Rotel drivers would be subject to all the terms and conditions of the current exemption, including its expiration date of July 30, 2010.
Commercial Driver's License (CDL) Standards; Volvo Trucks North America, Inc.'s Exemption Application
Document Number: E9-10208
Type: Notice
Date: 2009-05-05
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA previously announced its decision to renew Volvo Trucks North America, Inc.'s (Volvo) exemption for seven of its drivers to enable them to test-drive commercial motor vehicles (CMVs) in the United States without a commercial driver's license (CDL) issued by one of the States. FMCSA requested comment on the renewal of the exemption, but received no comments.
Airworthiness Directives; Pratt & Whitney (PW) JT9D-7R4 Series Turbofan Engines
Document Number: E9-10145
Type: Rule
Date: 2009-05-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) for PW JT9D-7R4 series turbofan engines. That AD currently requires removing certain reduced cooling flow 2nd stage high-pressure turbine (HPT) vane assemblies installed in certain 2nd stage HPT vane cluster assemblies. It also requires a visual and a fluorescent penetrant inspection (FPI) of the 2nd stage HPT air seal assembly, part number (P/N) 815097. This AD requires a visual and FPI of all P/N 2nd stage HPT air seal assemblies that were used with reduced cooling flow 2nd stage HPT vane assemblies. This AD results from PW identifying additional P/N air seal assemblies that are affected by the unsafe condition. We are issuing this AD to prevent uncontained failure of the 2nd stage HPT air seal assembly, leading to engine in-flight shutdown and damage to the airplane.
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