Federal Aviation Administration September 4, 2009 – Federal Register Recent Federal Regulation Documents
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Design Maneuvering Speed Limitation Statement
The Federal Aviation Administration proposes to amend the airworthiness standards applicable to transport category airplanes to clarify that flying at or below the design maneuvering speed does not allow a pilot to make multiple large control inputs in one airplane axis or single full control inputs in more than one airplane axis at a time without endangering the airplane's structure. This proposed regulation is the result of an accident investigation and responds to a National Transportation Safety Board recommendation. The results of the accident investigation indicate that many pilots might have a general misunderstanding of what the design maneuvering speed (VA) is and the extent of structural protection that exists when an airplane is operated at speeds below its VA. This action is being taken to prevent this misunderstanding from causing or contributing to a future accident.
Twelfth Joint Meeting, RTCA Special Committee 205/EUROCAE WG 71: Software Considerations in Aeronautical Systems
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 205/EUROCAE WG 71: Software Considerations in Aeronautical Systems.
Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR 21.151 and 21.153. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.
Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR 21.435 (c). The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.
Airworthiness Directives; Bombardier Model DHC-8-400 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:
Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes
We propose to adopt a new airworthiness directive (AD) for all McDonnell Douglas Model MD-90-30 airplanes. This proposed AD would require repetitive inspections for cracking of the overwing frames at stations 883, 902, 924, 943, and 962, left and right sides, and corrective actions if necessary. This proposed AD results from reports of cracked overwing frames. We are proposing this AD to detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane.
Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:
Airworthiness Directives; Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 Series Airplanes; and Model A340-211, -212, -213, -311, -312, and -313 Series Airplanes; and A340-541 and -642 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. 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 Opportunity To Participate, Criteria Requirements and Application Procedure for Participation in the Military Airport Program (MAP).
In anticipation of Congress enacting a reauthorization of the Airport Improvement Program (AIP) the FAA is publishing this annual notice. This notice announces the criteria, application procedures, and schedule to be applied by the Secretary of Transportation in designating or redesignating, and funding capital development annually for up to 15 current (joint-use) or former military airports seeking designation or redesignation to participate in the MAP. While FAA currently has continuing authority to designate or redesignate airports, FAA does not have authority to issue grants for fiscal year 2010 MAP, and will not have authority until Congress enacts legislation enabling FAA to issue grants.
Airworthiness Directives; Agusta S.p.A. Model AB412 and AB412 EP Helicopters
We are adopting a new airworthiness directive (AD) for the specified Agusta S.p.A. (Agusta) Model AB412 and AB412 EP helicopters. This AD results from mandatory continuing airworthiness information (MCAI) issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI establishes a life limit for certain rescue hoist cable assemblies and introduces the term ``hoist lift'' for determining cable life instead of the term ``hoist cycle.'' The MCAI also establishes a replacement time for each affected rescue hoist cable assembly (hoist cable assembly) for which the accumulated number of ``hoist cycles'' cannot be determined. The actions are intended to prevent failure of a hoist cable and inadvertent loss of a load.
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