Department of Transportation August 21, 2006 – Federal Register Recent Federal Regulation Documents
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Special Conditions: Airbus Model A380-800 Airplane, Crashworthiness
These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Many of these novel or unusual design features are associated with the complex systems and the configuration of the airplane, including its full-length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding crash survivability. 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. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
Special Conditions: Airbus Model A380-800 Airplane, Airplane Jacking Loads
These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Many of these novel or unusual design features are associated with the complex systems and the configuration of the airplane, including its full-length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding airplane jacking loads. 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. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
Special Conditions: Airbus Model A380-800 Airplane, Extendable Length Escape System
These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Many of these novel or unusual design features are associated with the complex systems and the configuration of the airplane, including its full-length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding extendable length escape slides. 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. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
Special Conditions: Airbus Model A380-800 Airplane, Loading Conditions for Multi-leg Landing Gear
These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Many of these novel or unusual design features are associated with the complex systems and the configuration of the airplane, including its full-length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding loading conditions for multi-leg landing gear. 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. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
Airworthiness Directives; Boeing Model 757 Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 757 airplanes. This proposed AD would require inspecting certain power feeder wire bundles for damage, inspecting the support clamps for these wire bundles to determine whether the clamps are properly installed, and performing corrective actions if necessary. This proposed AD results from a report that a power feeder wire bundle chafed against the number six auxiliary slat track, causing electrical wires in the bundle to arc, which damaged both the auxiliary slat track and power feeder wires. We are proposing this AD to prevent arcing that could be a possible ignition source for leaked flammable fluids, which could result in a fire. Arcing could also result in a loss of power from the generator connected to the power feeder wire bundle, and consequent loss of systems, which could reduce controllability of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain EMBRAER Model ERJ 170 and ERJ 190 airplanes. This proposed AD would require repetitive inspections to detect damaged smoke seals in the aft avionics compartment, repair/replacement if any damage is found, and reinforcement if no damage is found. This proposed AD also would require eventual replacement of all smoke seals in the aft avionics compartment with new, improved seals having new part numbers, which would terminate the repetitive inspections. This proposed AD results from a report of damaged smoke seals in the aft avionics compartment of the affected airplanes. We are proposing this AD to prevent smoke from penetrating into the passenger cabin during a fire in the avionics compartment.
Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A and CL-601-3R) Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. This proposed AD would require implementing a corrosion prevention and control program (CPCP) either by accomplishing specific tasks or by revising the maintenance inspection program to include a CPCP. This proposed AD results from the determination that, as airplanes age, they are more likely to exhibit indications of corrosion. We are proposing this AD to prevent structural failure of the airplane due to corrosion.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ, -135ER, -135KE, -135KL, and -135LR Airplanes; and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-135 and -145 series airplanes. This AD requires determining the torque values of the screws that attach the seat tracks to the airplane, and corrective action if necessary. This AD results from a report of undertorqued screws. We are issuing this AD to prevent improper torque of those screws, which in the case of a hard landing or a high deceleration impact condition could result in damage to the seat and possible subsequent injury to the passenger.
Airworthiness Directives; Boeing Model 777-200, -300, and -300ER Series Airplanes
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on June 16, 2006 (71 FR 34808). The error resulted in a reference only to the left main fuel tank in paragraph (f)(2) of that AD rather than to both the left and right main fuel tanks. This AD applies to certain Boeing Model 777-200, -300, and -300ER series airplanes. This AD requires a one-time inspection of the first bonding jumper aft of the bulkhead fitting to detect damage or failure and to determine the mechanical integrity of its electrical bonding path, and repair if necessary; measurement of the bonding resistance between the fitting for the fuel feed tube and the front spar in the left and right main fuel tanks, and repairing the bonding if necessary; and application of additional sealant to completely cover the bulkhead fittings inside the fuel tanks.
Airworthiness Directives; Aerospatiale Model ATR42-500 Airplanes and Model ATR72-212A Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Aerospatiale Model ATR42-500 and ATR72- 212A series airplanes, that requires repetitive inspections for cracking of the upper closing rib of the vertical fin, related investigative actions, and corrective actions if necessary. This new AD requires modifying the installation of the vertical leading edge fairing at the fin tip, which ends the repetitive inspections. This AD results from a report that rudder operation difficulties occurred on a Model ATR42-500 series airplane while the airplane was on the ground. We are issuing this AD to prevent interference between the upper closing rib and the rudder, which could result in a rudder jam and consequent reduced controllability of the airplane.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums 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; Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes
The FAA is adopting a new airworthiness directive (AD). The new AD is for Sandel Avionics Incorporated Model ST3400 TAWS/RMI units as described above. This AD requires installing a warning placard on the TAWS/RMI and revising the Limitations section of the airplane flight manual (AFM). This AD also requires installing upgraded software in the TAWS/RMI. This AD results from a report that an in-flight bearing error occurred in a Model ST3400 TAWS/RMI configured to receive bearing information from a very high frequency omnidirectional range (VOR) receiver interface via a composite video signal, due to a combination of input signal fault and software error. We are issuing this AD to prevent a bearing error, which could lead to an airplane departing from its scheduled flight path, which could result in a reduction in separation from, and a possible collision with, other aircraft or terrain.
Public Notice for Waiver of Aeronautical Land-Use Assurance Watertown Municipal Airport, Watertown, WI
The Federal Aviation Administration (FAA) is giving notice that a portion of the airport property containing 2.3 acres located at the southeast corner of Air Park Drive and Airport Rd. is not needed for aeronautical use as currently identified on the airport Layout Plan. This parcel was originally acquired through Grant No. AIP-01 in 1989. The parcel was an uneconomic remnant left from reconfiguration of a roadway intersection alongside the edge of the airport. The parcel is segregated from the airport and is not accessible from the air operations area. The land comprising this parcel is, therefore, no longer needed for aeronautical purposes. Income from the sale will be used to improve the airport. There are no impacts to the airport by allowing the airport to dispose of the property. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Public Notice for Waiver of Aeronautical Land-Use Assurance Freeman Municipal Airport, Seymour, IN
The Federal Aviation Administration (FAA) is giving notice that a portion of the airport (a northern portion of Parcel 5, 1.427 acres located northeast of the intersection of First Avenue and G Avenue East, presently used for neither aeronautical or agricultural use) is not needed for aeronautical use, as shown on the Airport Layout Plan. There are no impacts to the airport by allowing the airport to dispose of the property. Parcel E was acquired in September 27, 1948, under Quit Claim Deed from the United States of America to the Seymour Aviation Commission (recorded in Deed Record 93, pp. 405-419 in the Recorder's Office of Jackson County, Indiana). In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose. The release of this portion of Parcel 5 will allow the Freeman Municipal Airport to sell the land to a manufacturing company currently leasing the adjacent property.
Agency Information Collection Activity Under OMB Review
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) revision of a current information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on March 15, 2006, Vol. 71, No. 50, page 13446-13447. Information is collected to provide services to aircraft in-flight and protection of persons/property on the ground.
Proposed Revision of Class E Airspace; Mountain Home, ID
This action proposes to revise Class E airspace at Mountain Home, ID, beginning at 1,200 feet above ground level (AGL), replacing the existing Class G uncontrolled airspace. This airspace action will accommodate the terminal environment transition between Salt Lake Air Route Traffic Control Center (ARTCC) and Mountain Home AFB Radar Approach Control (RAPCON) by placing aircraft in controlled airspace during the transfer of aircraft radar identification between the facilities. In addition, a review of the legal description revealed that it does not reflect the correct airport reference point (ARP) of Mountain Home Municipal Airport and geographic position of the Sturgeon Non-Directional Beacon (NDB). This action will correct those minor discrepancies.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Detroit Metropolitan Wayne County Airport, Detroit, MI
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the Detroit Metropolitan Wayne County Airport (DTW) from aeronautical use to non-aeuronautical use and to authorize the sale of the airport property .The proposal consists of a land exchange between the Wayne County Airport Authority (WCAA) and the City of Romulus (City) for the Romulus Department of Public Works (DPW) property. The Runway 4L/22R construction project at DTW necessitated the WCAA acquire the City DPW site on Goddard Road (Parcel 65). A Memorandum of Understanding between the WCAA and the City provided that the WCAA construct a replacement DPW facility on surplus airport property West of relocated Wayne Road and then exchange this property (portions of seven parcels) for the former City DPW site. The new DPW facility has been constructed and the WCAA/City desire to complete the property exchange. The WCAA has requested from FAA a ``Release from Federal agreement obligated land covenants'' to complete the land exchange. The property proposed for release was acquired by the WCAA under FAA Project Numbers: 3-26-0026-1991, 3-26-0026-2292, 3-26-0026-3695, 3-26-0026- 4197, and 3-26-0026-4398. There are no impacts to the airport by allowing the WCAA to exchange property with the City. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal of the airport property will be in accordance with FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Pubic Notice for Waiver of Aeronautical Land-Use Assurance; Detroit Metropolitan Wayne County Airport, Detroit, MI
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the Detroit Metropolitan Wayne County Airport (DTW) from aeronautical use to non-aeronautical use and to authorize the sale of the airport property. The proposal consists of the sale of vacant, unimproved land owned by the Wayne County Airport Authority (WCAA). The WCAA has requested from FAA a ``Release from Federal agreement obligated land covenants'' to sell portions of six (6) parcels. The property proposed for release was acquired by the WCAA and FAA Project Numbers: 3-26-0026-1991, 3-26-0026-2292, 3-26-0026-3695, 3-0026-4197, and 3-26-0026-4398. There are no impacts to the airport by allowing the WCAA to dispose of the vacant property. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal of the airport property will be in accordance FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Notice of Opportunity for Public Comment on Surplus Property Release at Northeast Alabama Regional Airport, Gadsden, AL
Under the provisions of Title 49 U.S.C. 47153(c), notice is being given that the FAA is considering a request from the Gadsden Airport Authority to waive the requirement that a .98-acre parcel of surplus property, located at the Northeast Alabama Regional Airport, be used for aeronautical purposes.
Notice of Opportunity for Public Comment on Surplus Property Release at Northeast Alabama Regional Airport, Gadsden, AL
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 Gadsden Airport Authority to waive the requirement that a 24.4-acre parcel of surplus property, located at the Northeast Alabama Regional Airport, be used for aeronautical purposes.
Notice of Opportunity for Public Comment on Surplus Property Release at Northeast Alabama Regional Airport, Gadsden, AL
Under the provisions of Title 49, U.S.C. 47153(c), notice is being given that the FAA is considering a request from the Gadsden Airport Authority to waive the requirement that a 26.69-acre parcel of surplus property, located at the Northeast Alabama Regional Airport, be used for aeronautical purposes.
Disadvantaged Business Enterprises; Western States Guidance for Public Transportation Providers
This notice announces the Federal Transit Administration's (FTA) implementation of Department of Transportation guidance for participants of the Disadvantaged Business Enterprise (DBE) program. This notice solely concerns FTA implementation procedures applicable to FTA grantees in the states comprising the 9th Federal Judicial Circuit (California, Oregon, Washington, Alaska, Arizona, Idaho, Montana, Nevada, and Hawaii).
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