Department of Transportation June 19, 2009 – Federal Register Recent Federal Regulation Documents
Results 1 - 14 of 14
Hours of Service (HOS) of Drivers; Granting of Exemption; American Pyrotechnics Association (APA)
FMCSA announces its decision to grant the American Pyrotechnics Association (APA) exemption for 14 member motor carriers from FMCSA's regulation that drivers of commercial motor vehicles (CMV) may not drive after the 14th hour after coming on duty.
Hours of Service (HOS) of Drivers; Renewal of American Pyrotechnics Association (APA) Exemption From the 14-Hour Rule During Independence Day Celebrations
FMCSA previously announced its decision to renew the American Pyrotechnics Association (APA) exemption for 61 member motor carriers from FMCSA's regulation that drivers of commercial motor vehicles (CMVs) may not drive after the 14th hour after coming on duty. No comments were submitted to the public docket; consequently, the Agency confirms the renewal of the exemption.
Application of Air Excursions, LLC for Certificate Authority
The Department of Transportation is directing all interested persons to show cause why it should not issue an order finding Air Excursions, LLC, fit, willing, and able to engage in interstate scheduled air transportation of persons, property, and mail.
Airworthiness Directives; Fokker Model F28 Mark 0070 and 0100 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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:
Notice of Final Federal Agency Actions on Proposed Highway in California
This notice announces actions taken by the FHWA and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). These actions relate to a proposed highway project, replacement of the Antlers Bridge (Bridge No. 06-0089) and realignment of a 0.42-mile segment of Interstate 5, in the County of Shasta, State of California. Those actions grant licenses, permits, and approvals for the project.
Railroad Safety Advisory Committee (RSAC); Working Group Activity Update
The FRA is updating its announcement of RSAC's Working Group activities to reflect its current status.
Airworthiness Directives; Sikorsky Aircraft Corporation (Sikorsky) Model S-92A Helicopters
This document proposes adopting a new airworthiness directive (AD) for Sikorsky Model S-92A helicopters. The AD would require revising the Limitations section of the Rotorcraft Flight Manual (RFM) by clarifying that the Model S-92A helicopter was certificated as a transport category rotorcraft in both Categories A and B with different operating limitations for each category and must be operated accordingly. We have received reports that some operators are inappropriately operating Model S-92A helicopters using Category B limitations when the helicopter is configured with 10 or more passenger seats. Operating this helicopter when configured with 10 or more passenger seats and adhering to the less stringent limitations for the Category B configuration approved for a 9 or less passenger seat configuration does not maintain the FAA required minimum level of safety. This condition if not corrected, could result in operating under less stringent requirements.
Airworthiness Directives; Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 Series Airplanes
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; Piper Aircraft, Inc. PA-23, PA-31, and PA-42 Series Airplanes
We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) PA-23 series airplanes and all PA-31 and PA-42 series airplanes. This AD establishes life limits for safety- critical nose baggage door components. This AD also requires you to replace those safety-critical nose baggage door components and repetitively inspect and lubricate the nose baggage door latching mechanism and lock assembly. This AD results from several incidents and accidents, including fatal accidents, where the nose baggage door opening in flight was listed as a causal factor. We are issuing this AD to detect and correct damaged, worn, corroded, or non-conforming nose baggage door components, which could result in the nose baggage door opening in flight. The door opening in flight could significantly affect the handling and performance of the aircraft. It could also allow baggage to be ejected from the nose baggage compartment and strike the propeller. This failure could lead to loss of control.
Quarterly Rail Cost Adjustment Factor
The Board has approved the third quarter 2009 rail cost adjustment factor (RCAF) and cost index filed by the Association of American Railroads. The third quarter 2009 RCAF (Unadjusted) is 0.938. The third quarter 2009 RCAF (Adjusted) is 0.426. The third quarter 2009 RCAF-5 is 0.403.
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the 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; Dornier Luftfahrt GmbH Models Dornier 228-100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, and Dornier 228-212 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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; BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to all BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ airplanes. That AD currently requires repetitive inspections for corrosion of frames 15, 18, 41, and 43 and applicable related investigative and corrective actions. The existing AD also provides an optional action that would extend the repetitive inspection interval. This new AD also requires a high frequency eddy current inspection for corrosion of the outer frame flanges and door hinge bosses of frames 15, 18, 41, and 43. This AD results from a report indicating that corrosion has been detected in the outer frame flanges and door hinge bosses during scheduled maintenance. We are issuing this AD to prevent reduced structural integrity of the airplane.
Airworthiness Directives; Airbus Model A300 Airplanes; Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310 Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to the airplanes identified above. That AD currently requires revising the FAA-approved maintenance program to include a new airplane maintenance manual task that specifies a detailed inspection after each ram air turbine (RAT) retraction. That existing AD also currently requires, for certain airplanes, a one-time inspection to detect breaks in the bottom flange fitting of the RAT and corrective actions, if necessary; for certain airplanes, an adjustment of the ejection jack; and, for certain other airplanes, replacement of the aluminum part with an improved steel part. This AD also continues to require certain actions for additional airplanes and revising the FAA-approved maintenance program to include procedures for replacing the RAT swivel coupling fork fitting with a new steel part only. This AD results from a report that an additional swivel coupling of the RAT yoke fitting was found cracked during the accomplishment of the requirements of the existing AD. We are issuing this AD to prevent misrigging of the ejection jack of the RAT and to ensure removal of any RAT yoke fitting made from aluminum material. Such conditions could result in a broken or cracked swivel coupling and consequent failure of the RAT yoke fitting, which could result in the loss of RAT function and possible loss of critical flight control systems in the event of certain emergency situations.
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