Department of Transportation November 4, 2011 – Federal Register Recent Federal Regulation Documents

Utah Southern Railroad Company, LLC-Change in Operators Exemption-Iron Bull Railroad Company, LLC
Document Number: 2011-28642
Type: Notice
Date: 2011-11-04
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; DASSAULT AVIATION Model MYSTERE-FALCON 900 Airplanes
Document Number: 2011-28578
Type: Proposed Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all DASSAULT AVIATION Model MYSTERE-FALCON 900 airplanes. 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:
Airworthiness Directives; The Boeing Company Model 777-200 and -300 Series Airplanes
Document Number: 2011-28568
Type: Proposed Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777-200 and -300 series airplanes. This proposed AD would require replacing certain single-tabbed bonding brackets in the airplane empennage with two-tabbed bonding brackets. This proposed AD would also require, for certain airplanes, installing new bonding jumpers, and measuring the resistance of the modified installation to verify resistance is within specified limits. This proposed AD was prompted by reports of two failures of the single- tabbed bracket on the rudder. We are proposing this AD to prevent failure of the bonding jumper bracket, which could result in loss of lightning protection ground path, which could lead to increased lightning-induced currents and subsequent damage to composite structures, hydraulic tubes, and actuator control electronics. In the event of a lightning strike, loss of lightning ground protection could result in the loss of control of the airplane.
Commercial Driver's License Information System State Procedures Manual, Release 5.2.0
Document Number: 2011-28517
Type: Rule
Date: 2011-11-04
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA amends the Federal Motor Carrier Safety Regulations (FMCSRs) to incorporate by reference the most recent edition of the American Association of Motor Vehicle Administrators, Inc.'s (AAMVA) Commercial Driver's License Information System (CDLIS) State Procedures Manual (the Manual) (Release 5.2.0). This final rule requires all State driver licensing agencies (SDLAs) to use this recent edition of the Manual to develop the process required to transmit, receive, record, and update information on a CDLIS driver record. This information includes, but is not limited to, the commercial driver's license (CDL) holder's physical description, commercial and noncommercial driving status, medical certification status, convictions, disqualifications and accidents. This final rule is intended to ensure the uniform application of CDLIS procedures among all States.
Airworthiness Directives; Bombardier, Inc. Airplanes
Document Number: 2011-28360
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes. 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:
Airworthiness Directives; Sicma Aero Seat Passenger Seat Assemblies, Installed on, But Not Limited to, ATR-GIE Avions de Transport Régional Airplanes
Document Number: 2011-28357
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Sicma Aero Seat Model 9401, 9402, 9404, 9405, 9406, 9407, 9408, and 9409 series passenger seat assemblies, installed on, but not limited to, ATR-GIE Avions de Transport R[eacute]gional Model ATR42 and ATR72 airplanes. 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:
Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell), Model 205A-1, 205B, 210, and 212 Helicopters
Document Number: 2011-28355
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
This amendment supersedes an existing airworthiness directive (AD) for Bell Model 205B and 212 helicopters with certain main rotor blade (blade) assemblies installed. That AD currently requires washing the upper and lower surfaces of each blade and visually inspecting the grip plates, doublers, and the remaining upper and lower surfaces of the blades in the area between blade stations 24.5 to 40 for an edge void, corrosion, or a crack. This amendment retains the requirements of that AD for the affected part-numbered blades but increases the scope and frequency of the inspections and expands the applicability to include the Model 205A-1 and 210 helicopters, additional blade part numbers, and all helicopter serial numbers for the affected helicopter models. This amendment also requires applying a light coat of preservative oil (C-125) to all surfaces of the blade in addition to the inspection areas as required in the existing AD. This amendment is prompted by an additional report of a fatigue crack on a blade installed on a Model 212 helicopter. The actions specified by this AD are intended to detect an edge void, corrosion, or a crack on a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.
Agency Information Collection Activities: Request for Comments; Clearance of a New Information Collection; U.S. DOT Mentor Protégé Pilot Program
Document Number: 2011-27916
Type: Notice
Date: 2011-11-04
Agency: Office of the Secretary, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, Public law 104-13 (44 U.S.C. 3501 et seq) this notice announces the information collection request on Mentor Prot[eacute]g[eacute] Pilot Program annual report form, and the Mentor Prot[eacute]g[eacute] Pilot Program evaluation form. DOT's Mentor-Prot[eacute]g[eacute] Pilot Program enhances the capability of disadvantaged and small business owners to compete more successfully for federal procurement opportunities. The program encourages private-sector relationships and expands DOT's efforts to identify and respond to the developmental needs of small and disadvantaged businesses. The program is administered by the DOT OST Office of Small and Disadvantaged Business Utilization (OSDBU).
Airworthiness Directives; Eurocopter Deutschland GmbH (ECD) Model MBB-BK 117 C-2 Helicopters
Document Number: 2011-27776
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for ECD Model MBB-BK 117 C-2 helicopters. This action requires revising the Rotorcraft Flight Manual (RFM) by inserting certain temporary pages into the Emergency and Performance Data sections of the RFM to alert the operators to monitor the power display when a generator is deactivated and provides appropriate actions. This amendment is prompted by reports of too high a current flow when one generator is deactivated. The actions specified in this AD are intended to prevent failure of the remaining generator when one generator is deactivated, loss of electrical power, loss of systems necessary for flight safety, and subsequent loss of control of the helicopter.
Airworthiness Directives; Agusta S.p.A. (Agusta) Model AB139 and AW139 Helicopters
Document Number: 2011-27772
Type: Rule
Date: 2011-11-04
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for the specified Agusta model helicopters. This action requires inspecting certain modules and related connectors for corrosion. If there is corrosion on the connectors, this AD requires cleaning the connectors before further flight. If there is corrosion on a module, before further flight, this AD requires replacing the module with an airworthy module. This AD also requires modifying the Number 2 Modular Avionic Unit (MAU) ventilation duct. This amendment is prompted by some in- flight emergencies due to internal corrosion of the MAU circuit card assemblies. The actions specified in this AD are intended to detect corrosion of certain modules to prevent the display of misleading data to the flight crew, disengagement of the flight director modes of the autopilot or other alert system, increased workload of the flight crew, and subsequent loss of control of the helicopter.
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