Department of Transportation September 11, 2006 – Federal Register Recent Federal Regulation Documents
Results 1 - 18 of 18
Special Conditions: Airbus Model A380-800 Airplane, Flotation and Ditching
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 flotation and ditching. These proposed 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, Escape Systems Installed in Non-Pressurized Compartments
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 escape systems installed in non-pressurized compartments. 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, Escape Systems Inflation Systems
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 escape system reliability. 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; Emergency Exit Arrangement-Outside Viewing
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 outside viewing from emergency exits. 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; Stairways Between Decks
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 stairways between decks. 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.
Qualification of Drivers; Exemption Applications; Vision
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 42 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemptions will provide a level of safety that will be equivalent to, or greater than, the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Availability of a Draft Environmental Assessment
The purpose of this Notice is to make available to the public the draft Environmental Assessment (EA) for the Nuclear Ship SAVANNAH decommissioning. The draft EA analyzes the impacts associated with the full nuclear decommissioning of the vessel.
Airworthiness Directives; Airbus Model A300 Airplanes; A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and A310 Airplanes
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to all Airbus airplanes identified above. The original NPRM would have required improving the routing of certain electrical wire bundles in certain airplane zones, as applicable to the airplane model. The original NPRM resulted from fuel system reviews conducted by the manufacturer. This action revises the original NPRM by removing certain requirements, extending the compliance time for a certain replacement, and specifies that the actions in this proposed AD are considered interim action until a terminating action for the removed requirements is approved and available. We are proposing this supplemental NPRM to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
This action withdraws a notice of proposed rulemaking (NPRM) that proposed a new airworthiness directive (AD), applicable to all Lockheed Model L-1011-385 series airplanes. That action would have required repetitive leak tests of the lavatory drain systems and repair, if necessary; installation of a lever lock cap, vacuum breaker check valve or flush/fill line ball valve on the flush/fill line; periodic seal changes; and replacement of ``donut'' type waste drain valves installed in the waste drain system. Since the issuance of the NPRM, the Federal Aviation Administration (FAA) has reviewed existing data and determined that, for airplanes without a history of engine damage resulting from ``blue ice,'' such as Lockheed Model L-1011-385 series airplanes, the hazard of ``blue ice'' to persons and property may be more appropriately addressed through means other than AD action. Accordingly, the proposed rule is withdrawn.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This proposed AD would require revising the Certification Maintenance Requirements and the Maintenance Review Board Report sections of the Canadair Regional Jet Maintenance Requirements Manual to include changes and additions to checks of the aileron power control units (PCUs) and a change to the interval of the backlash check of the aileron control system. This proposed AD results from a report that data collected from in-service airplanes show that approximately 19 percent of aileron backlash checks conducted at 4,000-flight-hour intervals reveal that aileron backlash wear limits are being exceeded. We are proposing this AD to prevent exceeded backlashes in both aileron PCUs, which, if accompanied by the failure of the flutter damper, could result in aileron vibration/flutter and reduced controllability of the airplane.
Standard Instrument Approach Procedures; Miscellaneous Amendments
This amendment amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed 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; Arrow Falcon Exporters, Inc. (Previously Utah State University); Firefly Aviation Helicopter Services (Previously Erickson Air-Crane Co.); California Department of Forestry; Garlick Helicopters, Inc.; Global Helicopter Technology, Inc.; Hagglund Helicopters, LLC (Previously Western International Aviation, Inc.); International Helicopters, Inc.; Precision Helicopters, LLC; Robinson Air Crane, Inc.; San Joaquin Helicopters (Previously Hawkins and Powers Aviation, Inc.) S.M.&T. Aircraft (Previously U.S. Helicopters, Inc., UNC Helicopter, Inc., Southern Aero Corporation, and Wilco Aviation); Smith Helicopters; Southern Helicopter, Inc.; Southwest Florida Aviation International, Inc. (Previously Jamie R. Hill and Southwest Florida Aviation); Tamarack Helicopters, Inc. (Previously Ranger Helicopter Services, Inc.); U.S. Helicopter, Inc. (Previously UNC Helicopter, Inc.); West Coast Fabrication; and Williams Helicopter Corporation (Previously Scott Paper Co.) Model HH-1K, TH-1F, TH-1L, UH-1
This amendment adopts a new airworthiness directive (AD) for the specified restricted category type-certificated helicopters. The AD requires a review of the helicopter records to determine the Commercial and Government Entity (CAGE) code of the tail rotor (T/R) slider. If the T/R slider is FAA approved or has a certain legible CAGE code, this AD requires no further action. If you cannot determine whether the T/R slider is FAA approved and it has no stamped CAGE code, an illegible stamped CAGE code, or an affected CAGE code, the AD also requires, before further flight and at specified intervals, magnaflux inspecting the T/R slider for a crack. If a crack is found, the AD requires, before further flight, replacing the T/R slider with an airworthy T/R slider. The AD also requires replacing the T/R slider with an airworthy T/R slider on or before accumulating 1,000 hours time-in-service (TIS) or on or before 12 months, whichever occurs first. This amendment is prompted by two accidents attributed to sub-standard T/R sliders that failed during flight. The actions specified by this AD are intended to prevent failure of a T/R slider, loss of T/R control, and subsequent loss of control of the helicopter.
Notice of Intent To Rule on Request To Release Airport Property at the Oneida-Scott Municipal Airport, Oneida, TN
The Federal Aviation Administration is requesting public comment on the release of land at the Oneida-Scott Municipal Airport in the City of Oneida, Tennessee. This property, approximately 18.08 acres, will change to a non-aeronautical use. This action is taken under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Policy Statement on Approval for 10-Minute Rated Takeoff Thrust/Power During Takeoff With One-Engine Inoperative (OEI) Under 14 CFR Part 23 and 14 CFR Part 33
The Federal Aviation Administration (FAA) announces the availability of policy for the approval for 10-minuted rated takeoff thrust/power during takeoff with one-engine inoperative (OEI) under 14 CFR parts 23 and 33.
Draft Environmental Impact Statement: Pulaski and Laurel Counties, KY
On July 10, 2006, we published the Notice of Availability for the Draft Environmental Impact Statement (DEIS) for the proposed interstate facility in the south-central portion of Kentucky, between the Somerset Northern Bypass (I-66) and London, KY. The comment period on the DEIS is being extended to October 9, 2006.
Public Notice for Waiver of Aeronautical Land-Use Assurance; Muskegon County Airport, Muskegon, MI
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the airport from aeronautical use to non- aeronautical use and to authorize the sale of the airport property. The vacant parcel is 33' by 960' (approximately 0.73 acres) lies on the south side of Porter Road between Martin and Henry Streets in Norton Shores, Michigan. The land was acquired under FAA Project No. 9-20- 0071-01. There are no impacts to the airport by allowing the airport to dispose of the property. Since the purchase of this parcel, the parcel has sat vacant. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the subject 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.
Air Traffic Procedures Advisory Committee
The FAA is issuing this notice to advise the public that a meeting of the 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.
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