Department of Transportation November 14, 2007 – Federal Register Recent Federal Regulation Documents
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Airworthiness Directives; Viking Air Limited Model DHC-6 Series 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:
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.
Determination of Foreign Reconstruction or Rebuilding of U.S.-Built Vessels That Participate in the Capital Construction Fund and Cargo Preference Programs
The Maritime Administration seeks public comment on what standards the Maritime Administration should apply when making determinations of foreign reconstruction of U.S.-built vessels that participate in the Capital Construction Fund program and foreign rebuilding of U.S.-built vessels that participate in the cargo preference program.
Solicitation of Applications for Fiscal Year (FY) 2008 Motor Carrier Safety Assistance Program (MCSAP) High Priority and New Entrant Grant Funding
FMCSA announces that it has published an opportunity to apply for FY2008 MCSAP High Priority and New Entrant grant funding on the grants.gov Web site (https://www.grants.gov).
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
This document extends the comment period for the above- referenced NPRM, which proposes the adoption of a new airworthiness directive (AD) that applies to certain Boeing Model 737-600, -700, - 700C, -800, and -900 series airplanes. The NRPM would require various repetitive inspections to detect cracks along the chemically milled steps of the fuselage skin or missing or loose fasteners in the area of the preventative modification or repairs, replacement of the time- limited repair with the permanent repair if applicable, and applicable corrective actions if necessary, which would end certain repetitive inspections. The NPRM results from a fatigue test that revealed numerous cracks in the upper skin panel at the chemically milled step above the lap joint. This extension of the comment period is necessary to ensure that all interested persons have ample opportunity to submit any written relevant data, views, or arguments regarding the NPRM.
Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
This document extends the comment period for the above- referenced NPRM, which proposes the adoption of a new airworthiness directive (AD) that applies to all McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes. The NPRM would require repetitive inspections for cracking of the overwing frames from stations 845 to 905 (MD-87 stations 731 to 791), left and right sides, and corrective actions if necessary. The NPRM results from reports of cracked overwing frames. This extension of the comment period is necessary to ensure that all interested persons have ample opportunity to submit any written relevant data, views, or arguments regarding the NPRM.
Airworthiness Directive; Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all Lockheed Model 382, 382B, 382E, 382F, and 382G series airplanes. This proposed AD would require revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage to tolerance rating for each structural significant item (SSI), doing repetitive inspections to detect cracks of all SSIs, and repairing cracked structure. This proposed AD results from a report of incidents involving fatigue cracking and corrosion in transport category airplanes that are approaching or have exceeded their design service objective. We are proposing this AD to maintain the continued structural integrity of the entire fleet of Model 382, 382B, 382E, 382F, and 382G series airplanes.
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