Federal Aviation Administration March 1, 2006 – Federal Register Recent Federal Regulation Documents
Results 1 - 4 of 4
Airworthiness Directives; Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series
The FAA proposes to adopt a new airworthiness directive (AD) for Sicma Aero Seat third occupant seat assemblies, 133 Series. This proposed AD would require visually inspecting the installation of the two headrest bushings and installing Mecanindus pins to secure the bushings. This proposed AD results from Sicma's determination that missing or incorrectly secured bushings could loosen and cause disengagement of the headrest from the seat during a high-energy stop of the airplane, possibly injuring the seat occupant. We are proposing this AD to prevent disengagement of the headrest from the seat during a high-energy stop of the airplane that could injure the seat occupant.
Modification of Class E Airspace; Scott City Municipal Airport, KS
This action amends Title 14 Code of Federal Regulations, part 71 (14 CFR 71) by revising the Class E airspace area at Scott City, KS. A review of the controlled airspace at Scott City, KS revealed that the area does not comply with the criteria for 700 feet above ground level (AGL) airspace required for diverse departures and does not reflect the current Scott City, KS Municipal Airport airport reference point (ARP). This action increases the radius of the existing controlled airspace at Scott City, KS and corrects the ARP in the legal description.
Amendments to Colored Federal Airways; AK
This action revokes Colored Federal Airway B-12, modifies three Colored Federal Airways B-4, R-50 and G-7, and establishes Colored Federal Airway R-4 in Alaska. These amendments remove all airways and routes off the Bishop, AK, Nondirectional Radio Beacon (NDB) in preparation for the NDB's eventual decommissioning from the National Airspace System (NAS).
Airworthiness Directives; Rolls-Royce plc RB211 Trent 500, 700 and 800 Series Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 500, 700, and 800 series turbofan engines. This AD requires inspecting all engines to determine those that are equipped with a suspect oil filler cap assembly. This AD also requires, within seven days of the effective date of this AD, an initial and repetitive check of oil cap security following oil servicing of multiple-engine airplanes having more than one suspect oil filler cap assembly installed. Finally, this AD requires replacing affected oil filler cap assemblies. This AD results from four in- service oil loss events since March 2005, following failures to properly install the oil tank filler cap after oil servicing. We are issuing this AD to prevent oil loss that could result in multiple engine in-flight shutdowns during a flight.
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