Department of Transportation February 26, 2009 – Federal Register Recent Federal Regulation Documents

Commercial Driver's License (CDL) Standards: Granting of Exemption; Volvo Trucks North America (Volvo)
Document Number: E9-4148
Type: Notice
Date: 2009-02-26
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to grant Volvo Trucks North America, Inc.'s (Volvo) application for an exemption for one of its drivers to enable him to test-drive commercial motor vehicles (CMVs) in the United States without a commercial driver's license (CDL) issued by one of the States. Volvo stated the exemption is needed to support a field test to meet future air quality standards and to test-drive Volvo prototype vehicles to verify results in ``real world'' environments. Its driver holds a valid CDL issued in Sweden but lacks the U.S. residency necessary to obtain a CDL issued by one of the States. FMCSA believes the knowledge and skills testing and training program that drivers must undergo to obtain a Swedish CDL ensures that their drivers will achieve a level of safety that is equivalent to, or greater than, the level of safety achieved without the exemption.
Qualification of Drivers; Exemption Applications; Vision
Document Number: E9-4147
Type: Notice
Date: 2009-02-26
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 12 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 exemption renewals will provide a level of safety that is equivalent to, or greater than, the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
FHWA Laboratory and Field Research; Agency Information Collection Activity Under OMB Review
Document Number: E9-4098
Type: Notice
Date: 2009-02-26
Agency: Federal Highway Administration, Department of Transportation
The FHWA invites the public to comment on our intention to request the Office of Management and Budget (OMB) to approve a new information collection. This collection is summarized below under SUPPLEMENTARY INFORMATION. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.
Agency Information Collection Activities: Request for Comments for New Information Collection; Truck Congestion Information Assessment
Document Number: E9-4097
Type: Notice
Date: 2009-02-26
Agency: Federal Highway Administration, Department of Transportation
The FHWA invites public comments about our intention to request the Office of Management and Budget's (OMB) approval for a new information collection, which is summarized below under SUPPLEMENTARY INFORMATION . We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.
Eighth Meeting, RTCA Special Committee 216: Aeronautical System Security
Document Number: E9-4075
Type: Notice
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 216: Aeronautical Systems Security.
Amendment of Class E Airspace; Roanoke Rapids, NC
Document Number: E9-4074
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E Airspace at Roanoke Rapids, NC, to accommodate Standard Instrument Approach Procedures (SIAPs) at Halifax County Airport. The controlled airspace previously associated with this airport was removed in anticipation of the airport's scheduled closure. The closure of Halifax County Airport has been delayed because the opening of its replacement, Halifax-Northampton Regional Airport, has been delayed. Controlled airspace is necessary for the safety and management of SIAPs and for Instrument Flight Rule (IFR) operations to the airport.
Amendment of Class E Airspace; Guam Island, GU, and Saipan Island, CQ
Document Number: E9-3905
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
This action removes, renames and expands the Class E airspace areas serving Guam International Airport, Anderson AFB and Saipan Island. Additionally, this action will revoke the Saipan Island Class E surface area since it is no longer required, and expands other controlled airspace areas to protect aircraft conducting instrument approaches to Saipan International Airport. The FAA is taking this action to enhance the safety and management of aircraft operations in the vicinity of the Northern Mariana Islands.
Amendment of Class D Airspace; Anderson AFB, GU; Guam International Airport, GU; and Saipan International Airports, CQ
Document Number: E9-3904
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
This action amends the legal descriptions for Anderson AFB, and the Guam and Saipan International Airports. The Guam Air Route Traffic Control Center personnel conducted a review of their airspace and determined that current airspace descriptions needed to be updated. These are editorial revisions to reflect name changes and to update coordinates of the facilities. The changes will not affect the current area boundaries, altitudes, or the times of designation.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
Document Number: E9-3826
Type: Notice
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR Part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) Model 4101 Airplanes
Document Number: E9-3782
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) that applies to certain British Aerospace (Jetstream) Model 4100 series airplanes. The existing AD currently requires an eddy current conductivity test to measure the conductivity of the upper splice plate of the wing, and related investigative and corrective actions if necessary. This AD revises the applicability to include additional airplanes. This AD results from reports of exfoliation corrosion of the upper splice plate of the wing. We are issuing this AD to detect and correct such corrosion, which could result in reduced structural integrity of the airplane.
Airworthiness Directives; Airbus Model A310 Series Airplanes
Document Number: E9-3765
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) that applies to all Airbus Model A310 series airplanes. That AD currently requires repetitive detailed inspections to detect cracks propagating from the fastener holes that attach the left- and right- hand pick-up angles at frame 40 to the wing lower skin and fuselage panel, and corrective actions if necessary. This new AD revises the intervals for accomplishing the repetitive detailed inspections and provides for an optional terminating modification for the repetitive inspections. This new AD also revises the applicability of the AD to remove certain airplanes. This AD results from mandatory continuing airworthiness information originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. We are issuing this AD to prevent reduced structural integrity of the airplane due to fatigue damage, and consequent cracking of the pick-up angles at frame 40.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
Document Number: E9-3621
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive internal eddy current and detailed inspections to detect cracked stringer tie clips; measuring the fastener spacing and the edge margin if applicable, and doing applicable corrective and related investigative actions. As a temporary alternative to doing the actions described previously, this AD requires repetitive external general visual inspections of the skin and lap joints and repetitive external eddy current sliding probe inspections, as applicable, of the lap joints for cracks and evidence of overload resulting from cracked stringer tie clips, and applicable corrective actions if necessary. This AD results from a report of several cracked stringer tie clips. We are issuing this AD to detect and correct multiple adjacent cracked stringer tie clips and damaged skin and frames, which could lead to the skin and frame structure developing cracks and consequent decompression of the airplane.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP Series Airplanes
Document Number: E9-3616
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747-100, 747-100B, 747- 200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series airplanes. That AD currently requires an inspection to determine if acceptable external skin doublers are installed at the stringer 6 (S-6) lap splices, between station (STA) 340 and STA 400. For airplanes without the acceptable external skin doublers, the existing AD also requires repetitive related investigative actions and corrective actions if necessary. The existing AD also provides an optional terminating modification for the repetitive related investigative actions. This new AD mandates the optional terminating modification. This AD results from a report of cracked fastener holes at the right S-6 lap splice between STA 340 and STA 380. We are issuing this AD to prevent cracking in the fuselage skin, which could result in rapid decompression and loss of structural integrity of the airplane.
Airworthiness Directives; General Electric Company CF6-45 and CF6-50 Series Turbofan Engines
Document Number: E9-3615
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-45 and CF6-50 series turbofan engines. This AD requires replacing certain forward and aft centerbodies of the long fixed core exhaust nozzle (LFCEN) assembly. This AD results from the engine manufacturer issuing new service information. We are issuing this AD to prevent the forward and aft centerbody of the LFCEN assembly from separating due to high imbalance engine conditions, leading to damage to the airplane.
Airworthiness Directives; Boeing Model 777 Airplanes
Document Number: E9-3367
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 777 airplanes. This AD requires installing software upgrades to the airplane information management system (AIMS) located in the flight compartment. This AD results from an investigation that revealed that detrimental effects could occur on certain AIMS software during flight. We are issuing this AD to prevent an unannunciated loss of cabin pressure. If an undetected loss of pressure event were to cause an unsafe pressure in the cabin, the flight crew could become incapacitated.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ Airplanes
Document Number: E9-3366
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
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:
Airworthiness Directives; Fokker F.28 Mark 0070 and 0100 Airplanes
Document Number: E9-3365
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing 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:
Airworthiness Directives; Bombardier Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) Airplanes and Model CL-600-2D24 (Regional Jet Series 900) Airplanes
Document Number: E9-3364
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
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:
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes
Document Number: E9-3272
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all Boeing Model 747 series airplanes. That AD currently requires repetitive detailed inspections of the aft pressure bulkhead for indications of ``oil cans'' and previous oil can repairs, and corrective actions if necessary. An oil can is an area on a pressure dome web that moves when pushed from the forward side. This new AD requires a reduced compliance time for the initial detailed inspection and revises the applicability. This AD results from a report that cracks in oil-canned areas were found during an inspection of the aft pressure bulkhead. We are issuing this AD to detect and correct the propagation of fatigue cracks in the vicinity of oil cans on the web of the aft pressure bulkhead, which could result in rapid decompression of the airplane and overpressurization of the tail section, and consequent loss of control of the airplane.
Airworthiness Directives; Boeing Model 767-200, -300, and -400ER Series Airplanes
Document Number: E9-3263
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 767 series airplanes. That AD currently requires a one-time inspection for missing, damaged, or incorrectly installed parts in the separation link assembly on the deployment bar of the emergency escape system on the entry or service door, and installation of new parts if necessary. This new AD requires replacing the separation link assembly on the applicable entry and service doors with an improved separation link assembly, and doing related investigative and corrective actions if necessary; and inspecting for discrepancies of the unloaded spring dimensions in the separation link assembly, and doing corrective actions if necessary. This AD also removes certain airplanes from the applicability. This AD results from reports that entry and service doors did not open fully during deployment of emergency escape slides, and additional reports of missing snap rings. We are issuing this AD to prevent failure of an entry or service door to open fully in the event of an emergency evacuation, which could impede exit from the airplane. This condition could result in injury to passengers or crewmembers.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: E9-3215
Type: Rule
Date: 2009-02-26
Agency: Department of Transportation, Federal Aviation Administration
This rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: E9-3213
Type: Rule
Date: 2009-02-26
Agency: Federal Aviation Administration, Department of Transportation
This establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
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