Department of Transportation 2006 – Federal Register Recent Federal Regulation Documents

Results 1,001 - 1,050 of 3,043
Government/Industry Aeronautical Charting Forum Meeting
Document Number: 06-7111
Type: Notice
Date: 2006-08-24
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the bi-annual meeting of the Federal Aviation Administration (FAA) Aeronautical Charting (ACF) to discuss informational content and design of aeronautical charts and related products, as well as instrument flight procedures development policy and design criteria.
RTCA Special Committee 205/EUROCAE Working Group 71: Software Considerations in Aeronautical Systems Fourth Joint Plenary Meeting
Document Number: 06-7110
Type: Notice
Date: 2006-08-24
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 205/EUROCAE Working Group 71: Software Considerations in Aeronautical Systems.
Passenger Train Emergency Systems
Document Number: 06-7099
Type: Proposed Rule
Date: 2006-08-24
Agency: Federal Railroad Administration, Department of Transportation
This NPRM is intended to further the safety of passenger train occupants through both enhancements and additions to FRA's existing requirements for emergency systems on passenger trains. In this NPRM, FRA proposes to enhance existing requirements for emergency window exits and to establish requirements for rescue access windows to evacuate passenger train occupants. FRA also proposes to enhance passenger train emergency system requirements by expanding the application of requirements that are currently applicable only to passenger trains operating at speeds in excess of 125 mph (Tier II passenger trains) to passenger trains operating at speeds at or below 125 mph (Tier I passenger trains); these proposed enhancements would require that Tier I passenger trains be equipped with public address and intercom systems for emergency communication and that passenger cars provide emergency roof access for use by emergency responders. FRA is proposing to apply certain of the requirements to both existing and new passenger equipment, while other requirements would apply to new passenger equipment only.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: E6-13974
Type: Notice
Date: 2006-08-23
Agency: Maritime Administration, Department of Transportation
As authorized by Pub. L. 105-383 and Pub. L. 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 2006-25655 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 Pub. L. 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: E6-13973
Type: Notice
Date: 2006-08-23
Agency: Maritime Administration, Department of Transportation
As authorized by Pub. L. 105-383 and Pub. L. 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 2006-25656 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 Pub. L. 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.
Maintenance and Repair Reimbursement Pilot Program
Document Number: E6-13971
Type: Proposed Rule
Date: 2006-08-23
Agency: Maritime Administration, Department of Transportation
The Maritime Administration (MARAD) is amending its regulations governing its pilot program for the reimbursement of costs of qualified maintenance and repair (M&R) of Maritime Security Program (MSP) vessels performed in United States shipyards. Under Public Law 109-163, the Secretary of Transportation, acting through the Maritime Administrator, is directed to implement regulations that, among other things, replace MARAD's voluntary M&R reimbursement program with a mandatory system. The notice of proposed rulemaking for this action was published in the Federal Register on February 8, 2006 (71 FR 6438). Several of the comments received argued that MARAD lacks authority to unilaterally add to existing MSP agreements the added obligation on the part of the MSP contractor to enter into an M&R Pilot Program agreement. In order to have a full airing of this fundamental issue, MARAD is hereby giving notice that we have decided to open a reply comment period for this rulemaking. Reply comments may address the issue highlighted above or any other issue raised in the original set of comments received in this docket.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
Document Number: E6-13964
Type: Proposed Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300 B2 and B4 series airplanes. This proposed AD would require revising the airplane flight manual (AFM) to include procedures for resetting the trim and pitch trim levers after each landing, determining which servomotor moves the pitch trim control wheel, and doing applicable other specified actions. This proposed AD also provides for optional terminating actions for those requirements. This proposed AD results from a report of a sudden nose-up movement after disengagement of the autopilot in cruise. We are proposing this AD to ensure that the flightcrew is aware of the procedures for resetting the trim and pitch trim levers after each landing and to prevent failure of the servomotors of the pitch trim systems during flight. Failure of the servomotors of the pitch trim systems could result in uncommanded nose-up movement of the control surface of the pitch trim systems after disengagement of the autopilot in cruise.
Notice of Order Extending Comment Period for Show-Cause; International Air Transport Association Tariff Conference Proceeding
Document Number: E6-13958
Type: Notice
Date: 2006-08-23
Agency: Office of the Secretary, Department of Transportation
The Department has directed all interested persons to show cause why it should not issue an order withdrawing its approval under 49 U.S.C. 41309 for an International Air Transport Association (``IATA'') agreement, the Provisions for the Conduct of the IATA Traffic Conferences, insofar as that agreement establishes tariff conferences whereby IATA's member carriers discuss and agree upon passenger fares and cargo rates for U.S.-Australia/Europe markets. The Department is extending the due date for comments on that order from August 21 to October 20, 2006. Replies will be due November 20, 2006.
Exemptions From Average Fuel Economy Standards; Passenger Automobile Average Fuel Economy Standards
Document Number: E6-13957
Type: Proposed Rule
Date: 2006-08-23
Agency: National Highway Traffic Safety Administration, Department of Transportation
This proposed decision responds to a petition filed by Spyker Automobielen B.V. (Spyker) requesting that it be exempted from the generally applicable average fuel economy standard of 27.5 miles per gallon (mpg) for model years 2006 and 2007, and that, for Spyker, lower alternative standards be established. In this document, NHTSA proposes that the requested exemption be granted to Spyker and that alternative standards of 18.9 mpg be established for MY's 2006 and 2007.
Procedures for Transportation Workplace Drug and Alcohol Testing Programs: Revision of Substance Abuse Professional Credential Requirement; Technical Amendments
Document Number: E6-13956
Type: Rule
Date: 2006-08-23
Agency: Office of the Secretary, Department of Transportation
The Department of Transportation is adding state-licensed or certified marriage and family therapists to the list of credentialed professionals eligible to serve as substance abuse professionals under subpart O of 49 CFR part 40. The Department is also making a series of technical amendments to its drug and alcohol testing procedural rule. The purpose of the technical amendments is to clarify certain provisions of the rule as well as address omissions and typographical errors which have been called to our attention since the publication of the final rule in December 2000.
Airworthiness Directives; RECARO Aircraft Seating GmbH & Co. (RECARO) Model 3410 Seats
Document Number: E6-13911
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain RECARO Model 3410 302, 303, 306, 307, 314, 316, 317, 791, 792, and 795 series seats. This AD requires replacing the existing attachment bolts for the seat belts with longer attachment bolts. This AD results from a report of short attachment bolts that don't allow enough thread to properly secure the locknuts. We are issuing this AD to prevent a seat belt from detaching due to a loose locknut and attachment bolt, which could result in injury to an occupant during emergency conditions.
Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines
Document Number: E6-13910
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
This amendment supersedes an existing airworthiness directive (AD), that is applicable to Rolls-Royce plc (RR) models RB211-535E4-37, RB211-535E437, RB211-535C-37, RB211-535E4-B-75, RB211-535E4-C, and RB211-22B-02 turbofan engines. That AD currently requires inspecting certain high pressure (HP) turbine discs, manufactured between 1989 and 1999, for cracks in the rim cooling air holes, and, if necessary, replacing the discs with serviceable parts. The manufacturer identified reaming-induced machining anomalies (RIMA) as the cause for the cracking. This amendment requires the same inspections, and reduces the compliance times for eddy current inspection (ECI) for the RR RB211- 22B-02 engines. This amendment results from the manufacturer reducing their recommended compliance times for inspections on RB211-22B-02 engines. We are issuing this AD to prevent possible disc failure, which could result in an uncontained engine failure and damage to the airplane.
Airworthiness Directives; Pratt & Whitney PW4077D, PW4084D, PW4090, and PW4090-3 Turbofan Engines
Document Number: E6-13909
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Pratt & Whitney (PW) PW4077D, PW4084D, PW4090, and PW4090-3 turbofan engines that were reassembled with certain previously used high pressure compressor (HPC) exit brush seal assembly parts and certain new or refurbished HPC exit diffuser air seal inner lands. This AD requires replacing the HPC exit inner and outer brush seal packs with new brush seal packs, or replacing the HPC exit brush seal assembly with a new HPC exit brush seal assembly. This AD results from a report of oil leaking into the high pressure turbine (HPT) interstage cavity and igniting, leading to an engine case penetration and engine in- flight shutdown. Although liberated engine parts did not penetrate the engine nacelle, we are issuing this AD to prevent uncontained engine failure, damage to the airplane, and injury to passengers.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: E6-13831
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) that applies to certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. The existing AD currently requires inspecting contactors 1K4XD, 2K4XD, and K4XA to determine the type of terminal base plate, and applying sealant on the terminal base plates, if necessary. This new AD revises the effective date of the existing AD. This AD results from incidents of short circuit failures of certain alternating current (AC) contactors located in the avionics bay. We are issuing this AD to prevent short circuit failures of certain AC contactors, which could result in arcing and consequent smoke or fire.
Airworthiness Directives; Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 Series Airplanes
Document Number: E6-13829
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes. This AD requires repetitive inspections of the fluorescent light tube assemblies of the cabin, lavatory, and sidewall, and corrective actions if necessary. This AD also provides for optional terminating action for the repetitive inspections. This AD results from reports of overheating due to arcing between the fluorescent tube pins and the lamp holder contacts. The tubes had not been properly seated during installation. We are issuing this AD to prevent fumes, traces of visible smoke, and fire at the fluorescent light tube assembly.
Airworthiness Directives; Boeing Model 767-400ER Series Airplanes and Model 777-200 and -300 Series Airplanes
Document Number: E6-13825
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767-400ER series airplanes and Model 777-200 and - 300 series airplanes. This AD requires, for certain airplanes, repetitive testing of the fill and safety fittings of the cargo fire extinguishing bottles in the forward cargo compartment for leaks; and repetitive application of a corrosion inhibiting compound (CIC) or replacement of the cargo fire extinguishing bottles with reworked fire extinguishing bottles, as necessary. For all airplanes, this AD requires replacement of the cargo fire extinguishing bottles with reworked fire extinguishing bottles, which ends the repetitive tests and CIC applications if applicable. This AD results from failure of the safety fittings for the cargo fire extinguishing bottles. We are issuing this AD to prevent failure of the safety fittings for the cargo fire extinguishing bottles due to corrosion, which could result in leakage of extinguishing agent. If a fire occurs in the cargo bay, the cargo fire extinguishing bottles could have less than enough extinguishing agent to control a fire.
Revision of Class E Airspace; Barter Island, AK
Document Number: E6-13803
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Barter Island, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and one amended SIAP. This rule results in revised Class E airspace established upward from 700 feet (ft.) and 1,200 ft. above the surface at Barter Island Airport, AK.
Canadian Charter Air Taxi Operators
Document Number: E6-13664
Type: Rule
Date: 2006-08-23
Agency: Office of the Secretary, Department of Transportation
DOT is updating its rule concerning Canadian charter air taxis to make the rule consistent with the 1995 U.S.-Canada bilateral aviation agreement. When promulgated in 1981, the rule comported with the 1974 U.S.-Canada bilateral aviation agreement governing non- scheduled air services. However, the rule has not been updated to reflect the more liberal 1995 bilateral. Consequently, the rule, in its current form, contains certain restrictions on Canadian charter air taxis that are contrary to the 1995 bilateral. This final rule eliminates or amends those provisions. It also makes several other technical changes to the rule and adds a provision making it clear that Canadian charter air taxis are exempt from the statutory requirement of foreign air carriers to file family assistance plans.
Modification of Class E Airspace; Half Moon Bay, CA
Document Number: 06-7062
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
This action modifies the Class E airspace area at Half Moon Bay, CA. The establishment of an Area Navigation (RNAV) Global Positioning System (GPS) Z Instrument Approach Procedure (IAP) to Runway (RWY) 30 to Half Moon Bay Airport, Half Moon Bay, CA has made this action necessary. Additional controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing this RNAV (GPS) ZIAP to RWY 30 at Half Moon Bay Airport. The intended effect of this action is to provide adequate controlled airspace for Instrument Flight Rules operations at Half Moon Bay Airport, Half Moon Bay, CA
Proposed Agency Information Collection Activities; Comment Request
Document Number: E6-13900
Type: Notice
Date: 2006-08-22
Agency: Federal Railroad 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 comment. The ICR describes the nature of the information collection and its expected burden. The Federal Register notice with a 60-day comment period soliciting comments on the following collection of information was published on June 16, 2006 (71 FR 34990).
PYCO Industries, Inc.-Feeder Line Application-Lines of South Plains Switching, Ltd. Co.; Keokuk Junction Railway Co.-Feeder Line Application-Lines of South Plains Switching, Ltd. Co.
Document Number: E6-13898
Type: Notice
Date: 2006-08-22
Agency: Surface Transportation Board, Department of Transportation
The Board accepts the application of PYCO Industries, Inc. (PYCO) to purchase the entirety of the rail lines of South Plains Switching, Ltd. Co. (SAW) in Lubbock, TX, as complete under 49 U.S.C. 10907 and 49 CFR 1151. The Board also sets a procedural schedule, including the date for the filing of competing feeder line applications to purchase the entirety of SAW's rail lines.
Environmental Impact Statement; East Link Project, WA
Document Number: E6-13896
Type: Notice
Date: 2006-08-22
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration and the Central Puget Sound Regional Transit Authority (Sound Transit) intend to prepare an Environmental Impact Statement (EIS) in accordance with the National Environmental Policy Act (NEPA) for Sound Transit's proposed 11 to 19- mile extension of the Central Link Light rail transit project from Seattle to the cities of Mercer Island, Bellevue, and Redmond, within King County, Washington. The EIS will also be prepared in accordance with the provisions of the recently enacted Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU), and with Washington's State Environmental Policy Act (SEPA). The purpose of this Notice of Intent is to alert interested parties regarding the plan to prepare the EIS, to provide information on the nature of the proposed transit project, to invite participation in the EIS process, including comments on the scope of the EIS proposed in this notice, and to announce that public scoping meetings will be conducted. The EIS will address the no action alternative and reasonable alternatives that meet the project purpose and need.
Aviation Proceedings, Agreements Filed the Week Ending August 4, 2006
Document Number: E6-13878
Type: Notice
Date: 2006-08-22
Agency: Office of the Secretary, Department of Transportation
Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
Document Number: E6-13826
Type: Proposed Rule
Date: 2006-08-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Airbus Model A318, A319, A320, and A321 airplanes. The existing AD currently requires repetitive detailed inspections of the inboard flap trunnions for any wear marks and of the sliding panels for any cracking at the long edges; and corrective actions if necessary. This proposed AD would add airplanes to the applicability in the existing AD and change the inspection type. This proposed AD results from a determination that certain airplanes must be included in the applicability of the AD, and that the inspection type must be revised. We are proposing this AD to detect and correct wear of the inboard flap trunnions, which could lead to loss of flap surface control and consequently result in the flap detaching from the airplane. A detached flap could result in damage to the tail of the airplane.
Agency Information Collection Activities; Request for Comment; Renewal of an Information Collection: Financial Responsibility for Motor Carriers of Passengers and Motor Carriers of Property
Document Number: E6-13794
Type: Notice
Date: 2006-08-22
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The FMCSA invites comments on its plan to request the Office of Management and Budget's (OMB) approval to renew an existing information collection. This information collection renewal will be used to assure that motor carriers of property and passengers maintain appropriate levels of financial responsibility to operate on public highways. This notice is required by the Paperwork Reduction Act of 1995.
Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes
Document Number: E6-13731
Type: Rule
Date: 2006-08-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F27 Mark 050 airplanes. This AD requires doing an initial inspection of the leading edge sections of the elevators to detect loose leading edges and to ensure that there is no gap between the sections and the front spar, and corrective actions if necessary. This AD also requires determining the type of leading edge installed on the elevators. For certain airplanes, this AD requires repetitive inspections until the modification of the leading edge sections of the elevators and the application of sealant, which would end the repetitive inspections. This AD results from reports that the leading edges of the elevators were found loose, although the fasteners were still in place; in one case a stud was broken. In addition, the fastener attachment holes were elongated and worn out, and fretting damage was found on the elevator front spar and balance weights. Investigation revealed that vibration, induced by the propeller slipstream, was the cause of these discrepancies; the stud failure was due to improper installation of the fasteners. We are issuing this AD to prevent jamming, restricting, or binding of the elevators due to loose or missing fasteners, which could make the movement of the elevator difficult and decrease aerodynamic control of the airplane.
Special Conditions: Airbus Model A380-800 Airplane, Crashworthiness
Document Number: E6-13796
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13789
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13780
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13779
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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.
Continental Tire North America, Grant of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-13778
Type: Notice
Date: 2006-08-21
Agency: National Highway Traffic Safety Administration, Department of Transportation
Airworthiness Directives; Boeing Model 757 Airplanes
Document Number: E6-13730
Type: Proposed Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13714
Type: Proposed Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13713
Type: Proposed Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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.
Reading Blue Mountain and Northern Railroad Company-Abandonment Exemption-in Schuylkill County, PA
Document Number: E6-13669
Type: Notice
Date: 2006-08-21
Agency: Surface Transportation Board, Department of Transportation
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
Document Number: E6-13653
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13652
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13651
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13590
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: E6-13447
Type: Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 06-7066
Type: Notice
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 06-7065
Type: Notice
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 06-7064
Type: Notice
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 06-7063
Type: Proposed Rule
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 06-7061
Type: Notice
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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
Document Number: 06-7060
Type: Notice
Date: 2006-08-21
Agency: Federal Aviation Administration, Department of Transportation
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.
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