Department of Transportation October 13, 2005 – Federal Register Recent Federal Regulation Documents
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Establishment of Organization Designation Authorization Program
This final rule establishes the Organization Designation Authorization (ODA) program. The ODA program expands the scope of approved tasks available to organizational designees; increases the number of organizations eligible for organizational designee authorizations; and establishes a more comprehensive, systems-based approach to managing designated organizations. This final rule also sets phaseout dates for the current organizational designee programs, the participants in which will be transitioned into the ODA program. This program is needed as the framework for the FAA to standardize the operation and oversight of organizational designees. The effect of this program will be to increase the efficiency with which the FAA appoints and oversees designee organizations, and allow the FAA to concentrate its resources on the most safety-critical matters.
Artisan Liens on Aircraft; Recordability
Consistent with Agency practice, this notice is issued to advise interested parties of the addition of the States of Idaho and Utah to the list of those thirty-three states from which the Aircraft Registration Branch (FAA Aircraft Registry), Mike Monroney Aeronautical Center, Oklahoma City, Oklahoma, will accept artisan liens for recordation. Since December 17, 1981, the Aeronautical Center Counsel has issued these notices in the Federal Register.
Establishment of Class E3 Airspace, Riverside March Field, CA
This action establishes a Class E3 airspace area at Riverside March Field, CA.
Revision of Class E Airspace; Cheyenne, WY
This final rule will revised Class E airspace at Cheyenne, WY. New Instrument Flight Rules (IFR) routes sequences from the en route environment to/from Cheyenne Regional Airport/Jerry Olson Field makes this proposal necessary. Additional controlled airspace extending upward from 1,200 feet above the surface is necessary for the safety of aircraft. This action also correct as an error in the geographic coordinates of the Cheyenne Very High Frequency Omnidirectional Range Colocated Tactical Air Navigation and the airport designation.
Operating Limitations at Chicago O'Hare International Airport
On July 18, 2005, the Federal Aviation Administration (FAA) issued an order to show cause, which solicited written views on extending for a second time the FAA's August 18, 2004, order limiting scheduled operations at O'Hare International Airport (O'Hare). The August 2004 order made effective a series of schedule adjustments that the air carriers individually agreed to during a scheduling reduction meeting. These agreements, in general, resulted in a voluntary peak- hour arrival rate at O'Hare of eighty-eight scheduled flights, with the exception of the 8 p.m. hourthe final peak hour of the daywhen the rate would not exceed ninety-eight scheduled arrivals. The FAA previously extended the effectiveness of the August 2004 order through October 29, 2005. This notice announces that the FAA Administrator has signed an order that further extends the August 2004 order through April 1, 2006. The text of the extension order is published below as supplementary information to this notice.
Establishment of Class E Airspace; Eagle, CO
This final rule will establish Class E airspace at Eagle, CO. Additional Class E airspace is necessary to accommodate aircraft using a new Instrument Landing System or Localizer Distance Measuring Equipment (ILS or LOC DME) Standard Instrument Approach Procedure (SIAP) at Eagle County Regional Airport. This change is necessary for the safety of Instrument Flight Rules (IFR) aircraft executing the new SIAP at Eagle County Regional Airport, Eagle, CO.
Modification of Class D and Class E Airspace; Salina Municipal Airport, KS; Correction
This action corrects errors in the legal description of Class D airspace in a direct final rule, request for comments that was published in the Federal Register on Friday July 29, 2005 (70 FR 43742).
Intent To Prepare an Environmental Impact Statement and To Conduct Scoping Meetings for the Proposed Relocation of Runway 11R/29L and Associated Development at the Tucson International Airport in Tucson, AZ
The Federal Aviation Administration (FAA) is issuing this notice to advise the public that an Environmental Impact Statement (EIS) will be prepared to assess the potential impacts of the proposed relocation of Runway 11R/29L and associated development at Tucson International Airport. To ensure that all significant issues related to the proposed action are identified, one (1) public scoping meeting and one (1) governmental agency scoping meeting will be held.
Special Conditions: Learjet Model 35, 35A, 36, and 36A Airplanes; High-Intensity Radiated Fields (HIRF)
These special conditions are issued for Learjet Model 35, 35A, 36, and 36A airplanes modified by Genesis 3 Engineering, Inc. These modified airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of dual Revue Thommen AG AD30 Air Data Display Units and dual J2, Inc. Air Data Computers that perform critical functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for the protection of these systems from the effects of high-intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Special Conditions: Learjet Model 35 Series; High-Intensity Radiated Fields (HIRF)
These special conditions are issued for Learjet Model 35 series airplanes modified by Avcon Industries Inc. These modified airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of new Kollsman 24771 Air data computers and Thommen AD30 displays. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for the protection of these systems from the effects of high-intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Special Conditions: Boeing Model 767-200, -300, and -300F Series Airplanes; High-Intensity Radiated Fields (HIRF)
These special conditions are issued for Boeing Model 767-200, -300, and -300F series airplanes modified by ABX Air, Inc. These modified airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of an Innovative Solutions and Support Flat Panel Display System that performs critical functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for the protection of these systems from the effects of high-intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Policy for Repair and Alteration of Rotating Turbine Engine Life Limited Parts
The Federal Aviation Administration (FAA) announces the availability of proposed policy for the repair and alteration of rotating turbine engine-life limited parts (RTE-LLPs). This proposed policy establishes that the FAA will treat all repairs and alterations of RTE-LLPs as major repairs and major alterations. We are also proposing that all RTE-LLP repair and alteration data must include a methodology to assess the life of the repaired or altered part and the continued operational safety of the repaired product. This proposed policy provides guidance for: (1) Technical substantiation for repair or alteration of RTE-LLPs; and (2) Aircraft Certification Offices (ACOs) and Designated Engineering Representatives to evaluate and approve repair and alteration data.
Airworthiness Directives; Bell Helicopter Textron Model 212, 412, and 412EP Helicopters
This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron (Bell) model helicopters modified with Aeronautical Accessories, Inc. (AAI), Supplemental Type Certificate (STC) SH2820SO or that have the affected AAI Parts Manufacturer Approval (PMA) parts installed. This action requires inspecting a certain part-numbered reservoir assembly adapter (adapter) for the counter bore depth (dimension D). If the dimension D of the adapter exceeds .860 inch, before further flight, this AD requires replacing the reservoir assembly and adapter with airworthy parts. This amendment is prompted by a report of a rupture of an adapter during nitrogen charging because of inadequate wall thickness for the operating pressures. The actions specified in this AD are intended to prevent the rupture of an adapter, uncontrolled jetting of pressurized gas from the nitrogen bottle, and subsequent injury to occupants or damage to the helicopter.
Airworthiness Directives; Boeing Model 757-200, -200CB, and -200PF Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757-200, -200CB, and -200PF series airplanes. This AD requires an inspection of each trailing edge flap transmission assembly to determine the part number and serial number, and related investigative and corrective actions and part marking if necessary. This AD results from a report indicating that cracked flap transmission output gears have been discovered during routine overhaul of the trailing edge flap transmission assemblies. We are issuing this AD to prevent an undetected flap skew, which could result in a flap loss, damage to adjacent airplane systems, and consequent reduced controllability of the airplane.
Airworthiness Directives; Boeing Model 757-200, -200PF, and -300 Series Airplanes, Powered by Pratt & Whitney PW2000 Series Engines
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757-200, -200PF, and -300 series airplanes, powered by Pratt & Whitney PW2000 series engines. This AD requires repetitive inspections for loose or damaged components of the support brackets and associated fasteners for the hydraulic lines located in the nacelle struts, and any related investigative and corrective actions. This AD results from reports of damage and subsequent failure of the support brackets and associated fasteners for the hydraulic lines located internal to the upper fairing cavity of the nacelle struts. We are issuing this AD to prevent such failure, which, in conjunction with sparking of electrical wires, failure of seals that would allow flammable fluids to migrate to compartments with ignition sources, or overheating of the pneumatic ducts beyond auto-ignition temperatures, could result in an uncontained fire.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires examining the airplane's maintenance records to determine if the main landing gear (MLG) has been overhauled and if Titanine JC5A (also known as Desoto 823E508) corrosion- inhibiting compound (``CIC'') was used during the overhaul. For airplanes for which the maintenance records indicate that further action is necessary, or for airplanes on which CIC JC5A may have been used during manufacture, this AD requires a one-time detailed inspection for discrepancies of certain components of the MLG, and corrective action if necessary. This AD results from twelve reports of severe corrosion on one or more of three components of the MLG. We are issuing this AD to prevent collapse of the MLG, or damage to hydraulic tubing or the aileron control cables, which could result in possible departure of the airplane from the runway and loss of control of the airplane.
Airworthiness Directives; Dowty Aerospace Propellers Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies
The FAA is superseding an existing airworthiness directive (AD) for Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4- 82-F/13 propeller assemblies. That AD currently requires initial and repetitive ultrasonic inspections of propeller hubs, part number (P/N) 660709201. This AD requires the same initial and repetitive ultrasonic inspections, but reduces the initial and repetitive compliance times for Type R334/4-82-F/13 propeller assemblies when used on Construcciones Aeronauticas, S.A. (CASA) 212 airplanes. This AD results from a report of a hub separation on a CASA 212 airplane. We are issuing this AD to prevent propeller hub failure due to cracks in the hub, which could result in loss of control of the airplane.
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