Federal Aviation Administration July 29, 2008 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Gliders
Document Number: E8-17369
Type: Proposed Rule
Date: 2008-07-29
Agency: Federal Aviation Administration, Department of Transportation
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.
Establishment of Class E Airspace; Venetie, AK
Document Number: E8-17075
Type: Rule
Date: 2008-07-29
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E8-16583
Type: Rule
Date: 2008-07-29
Agency: Federal Aviation Administration, Department of Transportation
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.