Federal Aviation Administration May 14, 2015 – Federal Register Recent Federal Regulation Documents
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Notice of Availability of a Draft Environmental Assessment
The Federal Aviation Administration (FAA) proposes to fund, construct, and operate a new Airport Traffic Control Tower (ATCT) and Base Building at the General Wayne A. DowningPeoria International Airport (PIA), Peoria, Illinois. The FAA's preferred alternative is to construct the ATCT at a location approximately 1,000 feet east of the PIA terminal building. The purpose of the proposed project is to improve operational efficiency, meet existing and future operational and administrative expansion requirements, and accommodate state-of-the-art equipment upgrades. The need for the project is to provide a replacement ATCT, as the existing ATCT was constructed as part of the original terminal building, which is planned to be demolished. A new ATCT and Base Building at PIA would be able to meet these needs. The FAA has prepared a Draft Environmental Assessment (DEA) in conformance with the requirements of the National Environmental Policy Act of 1969 (NEPA) and FAA Order 1050.1E, Environmental Impacts: Policies and Procedures. The DEA analyzes the potential environmental impacts that may result from construction and operation of the proposed new ATCT and Base Building at the proposed site, as well as the no action alternative (i.e., not constructing and operating the new ATCT).
Airworthiness Directives; Airbus Airplanes
We propose to supersede Airworthiness Directive (AD) 2004-20- 14, for all Airbus Model A300 B4-2C, B4-103, and B4-203 airplanes; and all Model A300 B4-600, B4-600R, and F4-600R series airplanes. AD 2004- 20-14 requires repetitive inspections to detect cracking of the splice fitting at fuselage frame (FR) 47 between stringers 24 and 26 (left- and right-hand sides), and corrective actions if necessary. Since we issued AD 2004-20-14, we have determined that the inspection compliance time and repetitive inspection interval must be reduced to allow timely detection of cracks in the splice fitting at fuselage FR 47. This proposed AD would reduce the inspection compliance time and repetitive inspection intervals, and add Model A300 C4-605R Variant F airplanes to the applicability. We are proposing this AD to detect and correct cracking of the splice fitting at fuselage FR 47, which could result in reduced structural integrity of the airplane.
Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France)
We propose to supersede airworthiness directive (AD) 2002-13- 11 for Eurocopter France (now Airbus Helicopters) Model EC120B helicopters. AD 2002-13-11 currently requires installing front and side covers on the cabin floor to protect the yaw control at both the pilot and co-pilot stations. Since we issued AD 2002-13-11, we have determined that the required actions should apply only to the cabin's right-hand pilot station. This proposed AD would retain the requirements of AD 2002-13-11 but for only the pilot station. These proposed actions are intended to prevent an object from sliding between the canopy and the cabin floor, loss of yaw control, and subsequent loss of helicopter control.
Establishment of Class E Airspace; Cypress, TX
This action corrects the effective date of a final rule published in the Federal Register of April 24, 2015, establishing Class E airspace at Dry Creek Airport, Cypress, TX.
Airworthiness Directives; The Boeing Company Airplanes
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes. This proposed AD was prompted by reports of unreliable performance of the fuel scavenge system. This proposed AD would require changing the main fuel tank water scavenge system, center fuel tank fuel scavenge system, certain electrical panels; related investigative actions, and corrective actions if necessary; and for certain airplanes, changing to give redundant control of the center override/jettison fuel pumps and main jettison fuel pumps. We are proposing this AD to prevent fuel exhaustion and subsequent power loss of all engines due to loss of capability to scavenge fuel in the center fuel tank.