Federal Aviation Administration February 28, 2008 – Federal Register Recent Federal Regulation Documents
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Drug Enforcement Assistance
The FAA is implementing changes to its airmen certification and aircraft registration requirements. Two years after this rule becomes effective, paper pilot certificates may no longer be used to exercise piloting privileges. Five years after this rule becomes effective, certain other paper airmen certificates, such as those of flight engineers and mechanics, may no longer be used to exercise the privileges authorized by those certificates. To exercise the privileges after those respective dates, the airmen must hold upgraded, counterfeit-resistant plastic certificates. Student pilot certificates, temporary certificates, and authorizations are not affected. In addition, those who transfer ownership of U.S.-registered aircraft have 21 days from the transaction to notify the FAA Aircraft Registry. Those who apply for aircraft registration must include their printed or typed name with their signature. These changes are responsive to concerns raised in the FAA Drug Enforcement Assistance Act. The purpose of the changes is to upgrade the quality of data and documents to assist Federal, State, and local agencies to enforce the Nation's drug laws.
Re-Registration and Renewal of Aircraft Registration
The FAA proposes to amend requirements concerning the registration of aircraft. This proposal is based on the need to increase and maintain the accuracy of aircraft registration information in the Civil Aviation Registry. The proposed procedures would ensure aircraft owners periodically provide information regarding changes in registration. These amendments would respond to the concerns of law enforcement and other government agencies and would provide more accurate, up-to-date aircraft registration information to all users of the Civil Aviation Registry database.
Airworthiness Directives; Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes
We are revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 777-200, -200LR, -300, and -300ER series airplanes. The original NPRM would have required revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness by incorporating new limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. The original NPRM would also have required the initial performance of certain repetitive inspections specified in the AWLs to phase in those inspections, and repair if necessary. The original NPRM resulted from a design review of the fuel tank systems. This action revises the original NPRM by reducing the initial compliance time of certain repetitive inspections, adding more airplanes, and referring to new service information. We are proposing this supplemental NPRM to prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; General Electric Company CF34-8C1/-8C5/-8C5B1/-8E5/-8E5A1, and CF34-10E Series Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-8C1/-8C5/-8C5B1/-8E5/-8E5A1, and CF34-10E series turbofan engines with certain part number (P/N) and serial number (SN) fuel metering units (FMU) installed. This AD requires a onetime test of the FMU for a miswired (reversed polarity) condition of the input wires to the overspeed solenoid. This AD results from the discovery of miswired FMU overspeed solenoids in the field. We are issuing this AD to prevent the engine from failing to shutdown during an overspeed which may lead to uncontained engine failure.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-300, -400, and -500 series airplanes. This AD requires repetitive inspections for cracking of the body buttock line (BBL) 0.07 floor beam between body station (BS) 651 and BS 676 and between BS 698 and BS 717, and related investigative and corrective actions if necessary. This AD also provides an optional terminating action for the repetitive inspections. This AD results from reports of cracking in the BBL 0.07 floor beam. We are issuing this AD to prevent failure of the main deck floor beams at certain body stations due to fatigue cracking, which could result in rapid decompression of the airplane.
Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This 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 A319, A320, and A321 Series Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; ATR Model ATR42 and ATR72 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 Airplanes, and Model DHC-8-400 Series Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; Boeing Model 767-200, -300, -300F, and -400ER Series Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 767-200, -300, and -300F series airplanes. That AD currently requires reworking the surface of the ground stud bracket of the left and right transformer rectifier units (TRUs) and the airplane structure mounting surface, and measuring the resistance from the bracket to the structure and the ground lugs to the bracket using a bonding meter. This new AD revises the applicability of the existing AD to include additional airplanes and requires, among other actions, installation of a new ground stud bracket using faying surface bonding. This AD results from a report of loss of all direct current (DC) power generation during a flight, due to inadequate electrical ground path between the ground bracket of the TRUs/main battery charger (MBC) and the structure. We are issuing this AD to prevent depletion of the main battery while in flight, resulting from the loss of both TRUs and the MBC, and consequent loss of all DC power, which could impact the safe flight and landing of the airplane due to the loss of function or malfunction of essential/critical systems and displays in the cockpit.
Notice of Intent To Rule on Change in Use of Aeronautical Property at Louisville International Airport, Louisville, KY
The FAA is requesting public comment on the request by the Louisville Regional Airport Authority to change a portion of airport property from aeronautical to non-aeronautical use at the Louisville International Airport, Louisville, Kentucky. The request consists approximately of 8.65 acres of formal release. This action is taken under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Notice of Opportunity for Public Comment on Release of Federal Property at Cartersville Airport, Cartersville, GA.
Under the provisions of Title 49, U.S.C. Section 47153(c), notice is being given that the FAA is considering a request from the CartersvilleBartow County Airport Authority to waive the requirement that 1.095 acres in fee simple of federal property, located at the Cartersville Airport, be used for aeronautical purposes.
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