Federal Aviation Administration January 4, 2005 – Federal Register Recent Federal Regulation Documents
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Airworthiness Directives; Airbus Model A330-223, -321, -322, and -323 Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A330-223, -321, -322, and -323 airplanes. This proposed AD would require repetitive inspections of the firewall of the lower aft pylon fairing (LAPF), and corrective actions if necessary. This proposed AD is prompted by reports of cracking of the LAPF firewall. We are proposing this AD to detect and correct this cracking, which could reduce the effectiveness of the firewall and result in an uncontrolled engine fire.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on December 9, 2004 (69 FR 71339). The docket number of the final rule was incorrectly cited as FAA-2004-19767. This AD applies to all EMBRAER Model EMB-135 and -145 series airplanes. This AD requires a one-time inspection of each passenger service unit (PSU) to determine the serial number of the printed circuit board (PCB) installed in each PSU, replacement of the PCB if necessary, related investigative actions, and other specified actions.
Airworthiness Directives; Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) 250-B and 250-C Series Turboprop and Turboshaft Engines
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) 250-B and 250-C series turboprop and turboshaft engines with certain part numbers (P/Ns) of compressor adaptor couplings manufactured by Alcor Engine Company (Alcor), EXTEX Ltd. (EXTEX), RRC, and Superior Air Parts (SAP) installed. This AD requires operators to remove from service affected compressor adaptor couplings. This AD results from nine reports of engine shutdown caused by coupling failure. We are issuing this AD to reduce the risk of failure of the compressor adaptor coupling and subsequent loss of all engine power.
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