Federal Aviation Administration February 18, 2005 – Federal Register Recent Federal Regulation Documents
Results 1 - 9 of 9
Airworthiness Directives; Rolls-Royce plc RB211 Trent 875, 877, 884, 884B, 892, 892B, and 895 Series Turbofan Engines
The FAA proposes to supersede an existing airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 875, 877, 884, 892, 892B, and 895 series turbofan engines. That AD currently requires repetitive application of dry film lubricant (DFL) to low pressure compressor (LPC) fan blade roots. This proposed AD would require the same actions but at more frequent intervals than the existing AD, add the Trent 884B engine to the list of engine models affected, add a fan blade part number (P/N) to the affected list of fan blades, and would relax the initial DFL repetitive application compliance time for certain fan blades that have never been removed from the disk. This proposed AD results from discovering DFL in worse condition than anticipated on fan blades fitted to disks previously run for a significant period. This proposed AD also results from the need to update the list of engine models affected, and to update the list of fan blade part numbers affected. We are proposing this AD to prevent LPC fan blade loss, which could result in an uncontained engine failure and possible aircraft damage.
Notice of Intent To Rule on Application (05-09-C-00-YKM) To Impose and Use, the Revenue From a Passenger Facility Charge (YKM) at Yakima Air Terminal-McAllister Field, Submitted By the Yakima Air Terminal-McAllister Field Board, Yakima Air Terminal-McAllister Field, Yakima, WA
The FAA proposes to rule and invites public comment on the application to impose and use, PFC revenue at Yakima Air Terminal McAllister Field under the provisions of 49 U.S.C. 40117 and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Rules of Practice in FAA Civil Penalty Actions
The FAA is amending the procedural regulations governing the assessment of civil penalties against persons other than individuals acting as pilots, flight engineers, mechanics or repairmen. The rules establish a clear separation of functions between those agency employees who prosecute civil penalty actions and those who advise the Administrator, acting as FAA decisionmaker, about appeals of decisions by Department of Transportation (DOT) administrative law judges (ALJs). Recent organizational changes in the Office of the Chief Counsel necessitate updating these regulations so they accurately reflect the Office's current structure and division of functions. We are also amending the rules to provide the FAA Civil Penalty Hearing Docket's new address, new instructions on filing of documents, and information about the availability of documents and FAA decisions via the Internet. We are amending the procedural rule governing appeals from initial decisions regarding applications for fees under the Equal Access to Justice Act (EAJA) to reinsert language that was inadvertently omitted during a previous revision.
Air Traffic Procedures Advisory Committee
The FAA is issuing this notice to advise the public that a meeting of the Federal Aviation Air Traffic Procedures Advisory Committee (ATPAC) will be held to review present air traffic control procedures and practices for standardization, clarification, and upgrading of terminology and procedures.
Receipt of Noise Compatibility Program Amendment; Austin-Bergstrom International Airport, Austin, TX
The Federal Aviation Administration (FAA) announces that it is reviewing a proposed amendment (second) for the noise compatibility program that was submitted for Austin-Bergstrom International Airport under the provisions of Title 49, U.S.C. Chapter 475 (hereinafter referred to as ``Title 49'') and 14 CFR part 150 by the city of Austin. This program was submitted subsequent to a determination by the FAA that associated noise exposure maps submitted under 14 CFR part 150 for Austin-Bergstrom International Airport were in compliance with applicable requirements effective on April 29, 2000. The original noise compatibility program was approved on November 7, 2000, and subseqently amended on February 11, 2004. The proposed update to the noise compatibility program will be approved or disapproved on or before August 10, 2005.
Standard Instrument Approach Procedures; Miscellaneous Amendments
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Airworthiness Directives; Dassault Model Falcon 10 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for all Dassault Model Falcon 10 series airplanes. This AD requires a temporary change to the airplane flight manual (AFM) to provide procedures to the flightcrew for touchdown using the main landing gear to avoid a three- point landing. This AD also requires repetitive inspections of the piston rod of the drag strut actuator of the nose landing gear (NLG) for cracks, which would terminate the AFM revision, and corrective actions if necessary. In addition, this AD provides for a terminating modification, which would end the repetitive inspections. This AD is prompted by reports of failure of the piston rod of the drag strut actuator of the NLG. The cause of such failure has been attributed to fatigue cracking caused by corrosion in the piston rod of the drag strut actuator. We are issuing this AD to prevent cracking and/or fracture of the piston rod of the drag strut actuator of the NLG, which could result in a gear-up landing, structural damage, and possible injury to passengers and crew.
Airworthiness Directives; Boeing Model 747-400, -400D, and -400F Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-400, -400D, and -400F series airplanes. This AD requires replacing at least one flap control unit (FCU) in the main equipment center with a new or modified FCU. This AD is prompted by a report indicating that, after takeoff, an airplane was required to return to the airport because the autopilot disengaged. The report also indicated that, after selecting flaps for landing, the flaps indication display did not indicate the flap setting, requiring the airplane to land in alternate flap mode. We are issuing this AD to prevent disconnection of autoland/autopilot functions and loss of primary flaps control and flaps indication display due to disengagement of all three FCUs at the same time, which could lead to a non-normal high speed landing with the flaps retracted, increased pilot workload, and possible runway departure at high speeds during landing.
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