Department of Transportation July 29, 2008 – Federal Register Recent Federal Regulation Documents
Results 1 - 8 of 8
Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Gliders
This document makes a correction to a proposed airworthiness directive (AD), which was published in the Federal Register on July 3, 2008 (73 FR 38160), and applies to certain Stemme GmbH & Co. KG (Stemme) Model S10-VT powered sailplanes. This document proposed to require replacement of the single ear clamps in the fuel system with improved design parts. The FAA incorrectly referenced the docket number of this proposed AD as ``FAA-2008-0685'' instead of ``FAA-2008-0788.'' This document corrects the docket number.
Notice of Final Federal Agency Actions on a Proposed U.S. Highway Project 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 the proposed replacement of the existing non-standard connector, from the southbound San Diego Freeway (Interstate-405 PM 39.4/40.5) to the northbound Ventura Freeway (U.S. Highway-101 PM 17.0/19.4), with an upgraded connector. The new 50 mph two-lane connector would replace the current 20 mph single-lane connector. The project area is located in the communities of Encino and Sherman Oaks, in the City of Los Angeles, in the County of Los Angeles, in the State of California.
Establishment of Class E Airspace; Venetie, AK
This action establishes Class E airspace at Venetie, AK to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs) and Obstacle Departure Procedures (ODPs). Two SIAPs and an ODP are being developed for the Venetie Airport at Venetie Alaska. This action establishes Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at the Venetie Airport, Venetie, AK.
Airworthiness Directives; Cessna Aircraft Company Models 175 and 175A Airplanes
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 175 and 175A airplanes. This AD requires you to check the airplane logbook to determine if the original engine mounting brackets have been replaced. If the original engine mounting brackets are still installed, this AD requires you to repetitively inspect those brackets for cracks and replace any cracked engine mounting bracket. After replacing all four original engine mounting brackets, no further action will be required by this AD. This AD was prompted by a report that the engine became detached from the firewall during landing on one of the affected airplanes. We are issuing this AD to detect and correct cracks in the engine mounting brackets, which could result in failure of the engine mounting bracket. This failure could lead to the engine detaching from the firewall.
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