Department of Transportation 2005 – Federal Register Recent Federal Regulation Documents

Results 1,351 - 1,400 of 3,378
Special Conditions: Airbus Model A380-800 Airplane; Emergency Exit Arrangement-Outside Viewing
Document Number: 05-15658
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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 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; Stairways Between Decks
Document Number: 05-15657
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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 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; Fire Protection
Document Number: 05-15656
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions for the Airbus A380- 800 airplane, which has novel and unusual design features, such as a full-length double deck passenger cabin and distributed electrical equipment bays. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding fire protection. 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, Ground Turning Loads
Document Number: 05-15655
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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 ground turning loads. 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, Transient Engine Failure Loads
Document Number: 05-15654
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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. Some of these novel or unusual design features are associated with the high bypass engines used on the Model A380. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding transient engine failure loads. 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.
Agency Information Collection Activity Under OMB Review
Document Number: 05-15652
Type: Notice
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
In compliance with the Paperwork Reduction act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for review and approval of the new collection. The ICR describes the nature of the information collection and the expected burden. The Federal Register notice with a 60-day comment period soliciting comments on the following collection of information was published on April 20, 2004 on page 21179.
Establishment of Class D Airspace; Pascagoula, MS
Document Number: 05-15651
Type: Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class D airspace at Pascagoula, MS. A Federal contract tower with a weather reporting system is being constructed at the Trent Lott International Airport. Therefore, the airport will meet the criteria for establishment of Class D airspace. Class D surface area airspace is required when the control tower is open to contain existing Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action will establish Class D airspace extending upward from the surface, to and including 2,500 feet MSL, within a 4.1-mile radius of the airport.
Intent To Prepare an Environmental Impact Statement and Hold Scoping Meetings for Sacramento International Airport, Sacramento, CA
Document Number: 05-15650
Type: Notice
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is issuing this notice to advise the public that a joint Environmental Impact Statement/Environmental Impact Report (EIS/EIR) will be prepared for proposed development included in the Sacramento County Airport Systems (SCAS) Master Plan (Master Plan) for Sacramento International Airport (SMF), Sacramento, California. To ensure that all significant issues related to the proposed action are identified, one (1) public scoping meeting and one (1) governmental and public agency scoping meeting will be held.
Special Conditions: Airbus Model A380-800 Airplane, Crashworthiness
Document Number: 05-15649
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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 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 Inflation Systems
Document Number: 05-15648
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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 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
Document Number: 05-15647
Type: Proposed Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions 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 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.
Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes
Document Number: 05-15588
Type: Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model 717-200 airplanes. This AD requires repetitively replacing and testing a certain relay in the passenger oxygen release system in the forward cabin. This AD results from reports of a failed relay in the passenger oxygen release system. We are issuing this AD to prevent failure of the relay, which could result in the oxygen masks failing to deploy and deliver oxygen to the passengers in the event of a rapid decompression or cabin depressurization.
Airworthiness Directives; Boeing Model 727 Airplanes
Document Number: 05-15587
Type: Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This AD requires determining whether any float switches are installed in the fuel tanks, and corrective actions if necessary. This AD results from reports of contamination of the fueling float switch by moisture or fuel, and chafing of the float switch wiring against the fuel tank conduit. We are issuing this AD to prevent such contamination and chafing, which could present an ignition source inside the fuel tank that could cause a fire or explosion.
Airworthiness Directives; Boeing Model 747-400 and 747-400D Series Airplanes
Document Number: 05-15586
Type: Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-400 and 747-400D series airplanes. This AD requires an inspection for corrosion and cracks of the station 980 upper deck floor beam, and repair and related investigative actions if necessary. This AD results from reports of corrosion under the cart lift threshold at the station 980 upper deck floor beam. We are issuing this AD to detect and correct such corrosion, which could result in a cracked or broken floor beam, extensive damage to adjacent structure, and possible rapid decompression of the airplane.
Airworthiness Directives; Learjet Model 23, 24, 25, 35, and 36 Airplanes
Document Number: 05-15585
Type: Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Learjet Model 23, 24, 25, 35, and 36 airplanes. That AD currently requires repetitive inspections to detect deterioration of both flappers of the tip tank in each wing of the airplane, and various follow-on actions. The existing AD also requires replacing the flappers with new flappers, and repetitively performing certain other follow-on actions. This new AD requires an inspection of the flappers and flapper assemblies of the tip tank in each wing or a review of the airplane maintenance records to determine the part numbers, and replacement of certain flappers or flapper assemblies if necessary, which ends the existing repetitive inspections. This AD results from numerous continual inspections and the approval of a new, improved flapper and flapper assembly. We are issuing this AD to prevent significant reduction in the lateral control of the airplane due to imbalance of the fuel loads in the wings of the airplane.
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: 05-15584
Type: Rule
Date: 2005-08-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747 airplanes. This AD requires modifying the inflation systems of the upper deck escape slides; single-piece off- wing escape ramps/slides; two-piece off-wing escape slides; and door 1, 2, 4, and 5 escape slides/rafts. This AD results from a report of 30- to 60-second delays in the inflation of escape slides/rafts. We are issuing this AD to prevent actuation delays in the inflation systems of the escape slides/rafts, which could result in delayed or failed deployment of escape slides/rafts during emergency evacuation of an airplane.
Performance of Advanced Crash Avoidance Systems; Request for Information
Document Number: 05-15614
Type: Notice
Date: 2005-08-08
Agency: National Highway Traffic Safety Administration, Department of Transportation
NHTSA has received requests asking us to extend the comment period for the notice requesting information and expressions of interest in the research program on the performance of advanced crash avoidance systems. NHTSA is seeking information from all sources for its Advanced Crash Avoidance Technologies Program (ACAT). The ACAT program seeks to determine the safety impact of new and emerging technologies that are intended to help drivers avoid crashes, reduce their severity, and prevent injuries. To provide interested persons additional time to prepare comments, we are extending the end of the comment period from August 18, 2005, to September 30, 2005. This extension will allow interested persons additional time to provide information.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310 Series Airplanes; Equipped With General Electric CF6-80A3 or CF6-80C2 Engines
Document Number: 05-15594
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus airplane models, as specified above. This proposed AD would require installing electro-pneumatic locking bar devices (TRAS lock systems) in the engine nacelles, installing a dedicated and shielded electrical circuit that is segregated from the existing thrust reverser control system, and performing related investigative/ corrective actions if necessary. This proposed AD is prompted by the manufacturer's reassessment of the thrust reverser systems in the Airbus airplane models specified above, which showed that the thrust reverser could inadvertently deploy in flight under certain conditions. We are proposing this AD to prevent inadvertent deployment of thrust reversers in flight, which could result in reduced controllability of the airplane.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
Document Number: 05-15593
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A300 B2 and B4 series airplanes. This proposed AD would require an inspection to determine the part number of all angle of attack (AOA) sensors, and repetitive replacement of the AOA sensors with new or overhauled AOA sensors if necessary. This proposed AD would also provide an optional terminating action for the repetitive replacements. This proposed AD is prompted by reports of several false stall warnings associated with stick-shaker activation, occurring during take-off. We are proposing this AD to prevent false stall warnings associated with stick-shaker activation, which could result in increased pilot workload as the pilot tries to determine the cause of the stall warning and possible reduction in the pilot's ability to control the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 Airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
Document Number: 05-15592
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain EMBRAER Model EMB-135 airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes. The existing AD currently requires repetitive inspections of the spring cartridges of the elevator gust lock system to determine if the lock washer projection correctly fits the slots in the cartridge flange, and corrective action if necessary. The existing AD also provides for interim optional terminating action for the repetitive inspections for certain airplanes. This proposed AD would retain the requirements of the existing AD, and provide for final terminating action for all affected airplanes. This proposed AD is prompted by reports of an improperly fitting lock washer causing the clevis of the spring cartridge in the electromechanical elevator gust lock system to become unscrewed. We are proposing this AD to prevent unscrewing of the spring cartridge clevis from jamming the elevator, which could lead to reduced controllability of the airplane.
Airworthiness Directives; Airbus Model A300 B4-620, A310-304, A310-324, and A310-325 Airplanes
Document Number: 05-15591
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300 B4-620, A310-304, A310-324, and A310-325 airplanes. This proposed AD would require installing fused adaptors between the external wiring harness and the in-tank wiring at the connectors on the fuel tank wall of the auxiliary center tank (ACT). This proposed AD is prompted by the results of fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent an ignition source in the ACT, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Meggitt Model 602 Smoke Detectors Approved Under Technical Standard Order (TSO) TSO-C1C and Installed on Various Transport Category Airplanes, Including But Not Limited to Aerospatiale Model ATR42 and ATR72 Airplanes; Boeing Model 727 and 737 Airplanes; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30 and DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes
Document Number: 05-15590
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain smoke detectors installed on various transport category airplanes. This proposed AD would require replacing the affected smoke detectors with modified smoke detectors. This proposed AD is prompted by a report indicating that the affected smoke detectors can ``lock up'' during electrical power transfer from the auxiliary power unit to the engines. We are proposing this AD to identify and provide corrective action for a potentially inoperative smoke detector and to ensure that the flightcrew is alerted in the event of a fire.
Airworthiness Directives; Gulfstream Model GV and GV-SP Series Airplanes
Document Number: 05-15589
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Gulfstream Model GV and certain Model GV-SP series airplanes. This proposed AD would require a one-time inspection of the left and right aileron and elevator actuators to determine the part and serial numbers of each actuator, repetitive inspections of suspect actuators to detect broken damper shafts, and replacement of any actuator having a broken damper shaft. This proposed AD would also require that operators report any broken damper shaft they find to the FAA. This proposed AD also would provide an optional terminating action for the repetitive inspection requirements of this proposed AD. This proposed AD is prompted by reports of broken or cracked damper shafts within the aileron and elevator actuator assemblies. We are proposing this AD to detect and correct broken damper shafts, which could result in locking of an aileron or elevator actuator (hard-over condition), which would activate the hard-over protection system (HOPS), resulting in increased pilot workload and consequent reduced controllability of the airplane.
Airworthiness Directives; Bell Helicopter Textron Model 206A and 206B Helicopters
Document Number: 05-15581
Type: Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron (Bell) Model 206A and 206B helicopters modified by Aeronautical Accessories, Inc. Supplemental Type Certificate (STC) SH1392SO with certain part-numbered high crosstubes. This amendment requires inspecting at specified time intervals and replacing any cracked crosstubes. This amendment is prompted by the discovery of a cracked high forward crosstube. The actions specified by this AD are intended to detect a crack in the crosstube which could lead to failure of the crosstube, collapse of the landing gear, and subsequent loss of control of the helicopter.
Proposed Establishment of Class C Airspace and Revocation of Class D Airspace, Orlando Sanford International Airport, FL; and Proposed Modification of the Orlando International Airport Class B Airspace Area, FL
Document Number: 05-15567
Type: Proposed Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class C airspace at the Orlando Sanford International Airport (SFB), FL; revoke the existing Sanford, FL, Class D airspace area; and modify the existing Orlando International Airport (MCO), FL, Class B airspace area. The FAA is proposing this action to improve the flow of air traffic, enhance safety, and reduce the potential for midair collision in the Orlando, FL, terminal area.
Service of Process on Foreign Manufacturers and Importers
Document Number: 05-15561
Type: Rule
Date: 2005-08-08
Agency: National Highway Traffic Safety Administration, Department of Transportation
This final rule amends NHTSA's regulation on service of process on foreign manufacturers and importers to clarify existing regulatory requirements by rephrasing the regulation in a plain language, question and answer format and inserting an appendix containing a suggested designation form for use by foreign manufacturers and their agents. It also will enhance communications between foreign manufacturers and the agency by spelling out existing requirements for providing notice to NHTSA of changes in company name, address and product names, and changing the office to which foreign manufacturers must submit designation and related documents to reflect organizational changes occurring since the regulation was adopted.
Request for Public Comments and Office of Management and Budget (OMB) Approval of an Existing Information Collection (2137-0593)
Document Number: 05-15560
Type: Notice
Date: 2005-08-08
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) described below has been forwarded to the Office of Management and Budget (OMB) for extension of currently approved collection. The ICR describes the nature of the information collection and the expected burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 23, 2005, [FR 70, page 29554].
Request for Public Comments and Office of Management and Budget (OMB) Approval of an Existing Information Collection (2137-0594)
Document Number: 05-15559
Type: Notice
Date: 2005-08-08
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) described below has been forwarded to the Office of Management and Budget (OMB) for extension of currently approved collection. The ICR describes the nature of the information collection and the expected burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on May 23, 2005, [FR 70, page 29553].
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals.
Document Number: 05-15558
Type: Notice
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Revision of VOR Federal Airways V-9, V-50, V-67, V-69, V-129, V-173 and V-233; and Jet Routes J-35, J-80, J-101 and J-137; Springfield, IL
Document Number: 05-15557
Type: Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
This action revises Very High Frequency Omni-directional Range (VOR) Federal Airways V-9, V-50, V-67, V-69, V-129, V-173 and V-233; and Jet Routes J-35, J-80, J-101 and J-137 over the Springfield, IL area. The FAA is taking this action due to the relocation of the Capital VOR/Tactical Air Navigation (VORTAC) and the renaming of the ``Capital VORTAC'' to the ``Spinner VORTAC'' to enhance the management of aircraft operations over the Springfield, IL area.
Revocation of Restricted Area R-7104; Vieques Island, PR
Document Number: 05-15556
Type: Rule
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
This action revokes Restricted Area R-7104, Vieques Island, PR. The U.S. Navy weapons range on Vieques Island has been permanently closed; therefore, restricted airspace is no longer required at that location. The FAA is taking this action to return restricted airspace to the National Airspace System.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals.
Document Number: 05-15552
Type: Notice
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Noise Exposure Map Notice; Columbia Metropolitan Airport, Columbia, SC
Document Number: 05-15551
Type: Notice
Date: 2005-08-08
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by Richland- Lexington Airport District for Columbia Metropolitan Airport under the provisions of 49 U.S.C. 47501 et seq. (Aviation Safety and Noise Abatement Act) and 14 CFR Part 150 are in compliance with applicable requirements.
Denial of Petition for Import Eligibility for 2003-2004 CF Moto CF125T-2 Motorcycles
Document Number: 05-15481
Type: Notice
Date: 2005-08-05
Agency: National Highway Traffic Safety Administration, Department of Transportation
Decision That Nonconforming 1997 Land Rover Defender 90 Multi-Purpose Passenger Vehicles Are Eligible for Importation
Document Number: 05-15480
Type: Notice
Date: 2005-08-05
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document announces a decision by the National Highway Traffic Safety Administration (NHTSA) that certain 1997 Land Rover Defender 90 multi-purpose passenger vehicles (MPVs) that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards (FMVSS) are eligible for importation into the United States because they are substantially similar to vehicles originally manufactured for importation into and sale in the United States and that were certified by their manufacturer as complying with the safety standards (the U.S. certified version of the 1997 Land Rover Defender 90 MPV), and they are capable of being readily altered to conform to the standards.
Notice of Receipt of Petition for Decision That Nonconforming 1997 Ford Mustang Passenger Cars Are Eligible for Importation
Document Number: 05-15479
Type: Notice
Date: 2005-08-05
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that 1997 Ford Mustang passenger cars that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards (FMVSS) are eligible for importation into the United States because (1) they are substantially similar to vehicles that were originally manufactured for sale in the United States and that were certified by their manufacturer as complying with the safety standards, and (2) they are capable of being readily altered to conform to the standards.
Notice of Receipt of Petition for Decision That Nonconforming 2005 Harley Davidson FX, FL, and XL Motorcycles Are Eligible for Importation
Document Number: 05-15478
Type: Notice
Date: 2005-08-05
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that 2005 Harley Davidson FX, FL, and XL motorcycles that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards (FMVSS) are eligible for importation into the United States because (1) they are substantially similar to vehicles that were originally manufactured for sale in the United States and that were certified by their manufacturer as complying with the safety standards, and (2) they are capable of being readily altered to conform to the standards.
Harmonization of Noise Certification Standards for Propeller-Driven Small Airplanes
Document Number: 05-15465
Type: Rule
Date: 2005-08-05
Agency: Federal Aviation Administration, Department of Transportation
This final rule amends FAA regulations regarding airplane noise certification standards. These changes are necessary to harmonize two technical items with international standards and provide uniform noise certification standards for airplanes certificated in the United States and Joint Aviation Authorities (JAA) countries. This amendment will simplify airworthiness approvals for import and export purposes. We anticipate that the changes to these two items will apply only to a small number of older-technology airplanes.
Special Conditions; Diamond Aircraft Industries, EFIS and Full Authority Digital Engine Control (FADEC) on the Diamond DA-42; Protection of Systems for High Intensity Radiated Fields (HIRF)
Document Number: 05-15463
Type: Rule
Date: 2005-08-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA published a document on June 30, 2005 (70 FR 37656) concerning final special conditions for Diamond Aircraft Industries on the Diamond DA-42. There was an error in the preamble of the special conditions in the reference to the docket number. This document contains a correction to the docket number.
Noise Exposure Map Notice, Memphis International Airport, Memphis TN
Document Number: 05-15462
Type: Notice
Date: 2005-08-05
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces the determination that the noise exposure maps submitted by Memphis-Shelby County Airport Authority for Memphis International Airport under the provisions of 49 U.S.C. 47501 et seq (Aviation Safety and Noise Abatement Act) and 14 CFR Part 150 are in compliance with applicable requirements.
Amendment of Class E Airspace; Brunswick, ME; Correction
Document Number: 05-15461
Type: Rule
Date: 2005-08-05
Agency: Federal Aviation Administration, Department of Transportation
This action corrects a final rule published in the Federal Register on May 25, 2005 (70 FR 29943-29944). In that rule, the description of the designated airspace contained errors and omissions. Action to correct these errors and omissions result in a delay of the effective date. This action corrects the final rule and effective date. The correct effective date is October 27, 2005.
Disclosure of Code-Sharing and Long-Term Wet Lease Arrangements
Document Number: 05-15426
Type: Rule
Date: 2005-08-04
Agency: Office of the Secretary, Department of Transportation
This action amends the rule governing the disclosure of code- share and long-term wet lease arrangements in print advertisements of scheduled passenger services to permit carriers to disclose generically that some of the advertised service may involve travel on another carrier, so long as they also identify a list of all potential carriers involved in serving the markets advertised. The action is taken in response to a petition for rulemaking filed by United Airlines, Inc.
Proposed Agency Information Collection Activities; Comment Request
Document Number: 05-15418
Type: Notice
Date: 2005-08-04
Agency: Federal Railroad Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995 and its implementing regulations, the Federal Railroad Administration (FRA) hereby announces that it is seeking approval of the following information collection activities. Before submitting these information collection requirements for clearance by the Office of Management and Budget (OMB), FRA is soliciting public comment on specific aspects of the activities identified below.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: 05-15416
Type: Notice
Date: 2005-08-04
Agency: Maritime Administration, Department of Transportation
As authorized by Public Law 105-383 and Public Law 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2005-21996 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Public Law 105-383 and MARAD's regulations at 46 CFR Part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR Part 388.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: 05-15415
Type: Notice
Date: 2005-08-04
Agency: Maritime Administration, Department of Transportation
As authorized by Public Law 105-383 and Public Law 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2005-21994 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines in accordance with Public Law 105-383 and MARAD's regulations at 46 CFR Part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR Part 388.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: 05-15414
Type: Notice
Date: 2005-08-04
Agency: Maritime Administration, Department of Transportation
As authorized by Public Law 105-383 and Public Law 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2005-21995 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Public Law 105-383 and MARAD's regulations at 46 CFR Part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR Part 388.
Information Collection Available for Public Comments and Recommendations
Document Number: 05-15413
Type: Notice
Date: 2005-08-04
Agency: Maritime Administration, Department of Transportation
In accordance with the Paperwork Reduction Act of 1995, this notice announces the Maritime Administration's (MARAD's) intention to request extension of approval for three years of a currently approved information collection.
Notice of Intent To Rule on Request To Release Airport Property at Chickasha Municipal Airport, Chickasha, OK
Document Number: 05-15404
Type: Notice
Date: 2005-08-04
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the release of land at Chickasha Municipal Airport under the provisions of Title 49 United States Code, Section 47153.
Proposed Establishment of Class E Airspace; Deering, AK
Document Number: 05-15403
Type: Proposed Rule
Date: 2005-08-04
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish new Class E airspace at Deering, AK. Four new Standard Instrument Approach Procedures (SIAPs) are being published for the Deering Airport. There is no existing Class E airspace to contain aircraft executing the new instrument procedures at Deering, AK. Adoption of this proposal would result in the establishment of Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Deering, AK.
Proposed Establishment of Class E5 Airspace; Gardner, KS
Document Number: 05-15402
Type: Proposed Rule
Date: 2005-08-04
Agency: Federal Aviation Administration, Department of Transportation
This document proposes to establish Class E5 airspace at Gardner, KS.
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