Federal Aviation Administration January 19, 2010 – Federal Register Recent Federal Regulation Documents
Results 1 - 9 of 9
Sixteenth Plenary Meeting: RTCA Special Committee 203: Unmanned Aircraft Systems
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 203: Unmanned Aircraft Systems.
Thirteenth Plenary 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. 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; Turbomeca Turmo IV A and IV C Turboshaft Engines
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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 Corporation Model DC-10-10, DC-10-10F, and MD-10-10F Airplanes
We propose to adopt a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-10-10, DC-10-10F, and MD-10-10F airplanes. This proposed AD would require a one-time high frequency eddy current inspection of fastener holes for cracks at the left and right side wing rear spar lower cap at station Xors=345, and other specified and corrective actions if necessary. This proposed AD results from a report of three instances of Model DC-10-10F airplanes having fuel leaks in the wing rear spar lower cap at station Xors=345. We are proposing this AD to prevent cracks in the spar cap, which if not corrected could lead to cracking of the lower wing skin, fuel leaks, and the inability of the structure to sustain limit load.
Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/SF340A) and SAAB 340B Airplanes Modified in Accordance With Supplemental Type Certificate (STC) SA00244WI-D, ST00146WI-D, or SA984GL-D
The FAA proposes to adopt a new airworthiness directive (AD) for certain Saab AB, Saab Aerosystems Model SAAB 340A (SAAB/SF340A) and SAAB 340B airplanes. This proposed AD would require inspecting the fuselage surface for corrosion and cracking behind the external adapter plate of the antennae installation, and repair if necessary. This proposed AD results from a report of a crack found behind the external adapter plate of the antennae during inspection. Similar cracking was found on two additional airplanes, and extensive corrosion was found on one airplane. We are proposing this AD to detect and correct corrosion and cracking behind the external adapter plate of the antennae of certain safe-life structure, which could result in reduced structural integrity and consequent rapid depressurization of the airplane.
Airworthiness Directives; Sicma Aero Seat 88xx, 89xx, 90xx, 91xx, 92xx, 93xx, 95xx, and 96xx Series Passenger Seat Assemblies, Installed on Various Transport Category 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 Intent To Prepare an Environmental Assessment and Request for Public Scoping Comments for the Air Tour Management Plan Program at Death Valley National Park
The FAA, with NPS as a cooperating agency, has initiated development of an Air Tour Management Plan (ATMP) for Death Valley National Park (DEVA), pursuant to the National Parks Air Tour Management Act of 2000 (Public Law 106-181) and its implementing regulations (14 CFR Part 136, Subpart B, National Parks Air Tour Management). The objective of the ATMIP is to develop acceptable and effective measures to mitigate or prevent the significant adverse impacts, if any, of commercial air tour operations upon the natural resources, cultural resources, and visitor experiences of a national park unit and any tribal lands within or abutting the park. It should be noted that the ATMP has no authorization over other non-air-tour operations such as military and general aviation operations. In compliance with the National Environmental Policy Act of 1969 (NEPA) and FAA Order 1050.1E, an Environmental Assessment is being prepared.
Public Notice for Waiver of Aeronautical Land-Use Assurance Dupont-Lapeer Airport, Lapeer, MI
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the Dupont Lapeer Airport from aeronautical use to non-aeronautical use and to authorize the sale of the airport property. The proposal consists of the sale of vacant, unimproved land owned by the Dupont-Lapeer Airport Board (Board).
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