Department of Transportation May 2006 – Federal Register Recent Federal Regulation Documents

Petition for Waiver of Compliance
Document Number: E6-8315
Type: Notice
Date: 2006-05-31
Agency: Federal Railroad Administration, Department of Transportation
V&S Railway, LLC-Acquisition and Operation Exemption-The Hutchinson and Northern Railway Company
Document Number: E6-8259
Type: Notice
Date: 2006-05-31
Agency: Surface Transportation Board, Department of Transportation
Union Pacific Railroad Company-Abandonment Exemption-in Ouachita County, AR
Document Number: E6-8258
Type: Notice
Date: 2006-05-31
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Sikorsky Aircraft Corporation Model S-92A Helicopters
Document Number: 06-4911
Type: Rule
Date: 2006-05-31
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for the specified Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This action requires inspecting each main transmission assembly mounting bolt (bolt) for wear or corrosion, and if wear or corrosion is found, replacing the bolt, bolt barrel nut, and cage. This amendment is prompted by a report of a failure of a bolt that was discovered during a routine maintenance inspection. The actions specified in this AD are intended to prevent failure of a bolt, which could result in loss of support of the main transmission and subsequent loss of control of the helicopter.
Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 Airplanes
Document Number: 06-4910
Type: Rule
Date: 2006-05-31
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 airplanes. This AD requires revising the Limitations section of the airplane flight manual (AFM) by incorporating revised takeoff performance tables. This AD results from a correction of the power setting logic and table limits in the performance model by the engine manufacturer. We are issuing this AD to ensure that the flightcrew is provided with correct information to ensure a safe takeoff at certain altitudes; inadequate takeoff performance tables used in such conditions could result in reduced control of the airplane during takeoff.
Airworthiness Directives; Honeywell International Inc. T5311A, T5311B, T5313B, T5317A, T5317A-1, and T5317B Series Turboshaft Engines and Lycoming Former Military T53-L-11B, T53-L-11D, T53-L-13B, T53-L-13B/D, and T53-L-703 Series Turboshaft Engines
Document Number: 06-4908
Type: Rule
Date: 2006-05-31
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) for AlliedSignal, Inc. T5317A-1 turboshaft engines. That AD currently requires repetitive engine fuel pump pressure tests of certain fuel control regulator assemblies to determine if both fuel pumps in the fuel control regulator assemblies are producing fuel pressure. That AD also requires replacing the fuel control regulator assembly, if necessary. This AD requires initial and repetitive visual and dimensional inspections of fuel control regulator assembly main and secondary drive shaft and pump gear splines, installed in certain fuel control regulator assemblies. This AD also expands the engine applicability, and includes certain engines installed on helicopters certified under Sec. 21.25 or 21.27 of the Code of Federal Regulations (14 CFR 21.25 or 14 CFR 21.27). This AD results from several reports of loss of fuel flow from the engine fuel control regulator assembly due to failure of both main and secondary drive shaft and pump gear splines. We are issuing this AD to prevent in-flight engine failure and forced autorotation landing.
Organization and Delegation of Powers and Duties
Document Number: 06-4854
Type: Rule
Date: 2006-05-31
Agency: Office of the Secretary of Transportation, Department of Transportation
This amendment delegates various authorities vested in the Secretary of Transportation (Secretary) by the ``Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users'' or ``SAFETEA-LU'' (Pub. L. 109-59; August 10, 2005) and other laws to the Research and Innovative Technology Administrator, the Federal Highway Administrator, the Federal Railroad Administrator, the National Traffic Highway Safety Administrator, the Federal Transit Administrator, the Pipeline and Hazardous Materials Safety Administrator, the Federal Motor Carrier Safety Administrator, and the Under Secretary for Transportation Policy.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: 06-4472
Type: Rule
Date: 2006-05-31
Agency: Federal Aviation Administration, Department of Transportation
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.
Petitions for Exemption; Summary of Petitions Received
Document Number: E6-8295
Type: Notice
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Performance-Based Operations Aviation Rulemaking Committee
Document Number: E6-8293
Type: Notice
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
This document announces a public meeting in which the Federal Aviation Administration (FAA) and members of the Performance-Based Operations Aviation Rulemaking Committee (PARC) will discuss implementing the performance-based National Airspace System. The first day of the meeting will focus on performance-based operations. The second day of the meeting will focus on navigation infrastructure capabilities.
Petitions for Exemption; Summary of Petitions Received
Document Number: E6-8292
Type: Notice
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Petitions for Exemption; Summary of Petitions Received
Document Number: E6-8291
Type: Notice
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: E6-8290
Type: Rule
Date: 2006-05-30
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.
Notice of Request for the Extension of Currently Approved Information Collections
Document Number: E6-8289
Type: Notice
Date: 2006-05-30
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration invites public comments about our intention to request the Office of Management and Budget's (OMB) approval to renew the following information collections: (1) Nondiscrimination as it Applies to FTA Grant Programs. (2) Title VI as it Applies to FTA Grant Programs. The collections involve our Nondiscrimination and Title VI Programs. The information to be collected for the Nondiscrimination Program is necessary to ensure that any employee or applicant for employment is not discriminated against on the basis of race, color, creed, sex, national origin, age or disability. The information to be collected for the Title VI Program is necessary to ensure that service and benefits are provided nondiscriminatorily without regard to race, color, or national origin. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: E6-8287
Type: Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
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.
Revision of Class E Airspace; Atqasuk, AK
Document Number: E6-8284
Type: Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Atqasuk, AK to provide adequate controlled airspace to contain aircraft executing four amended Standard Instrument Approach Procedures (SIAPs). This rule results in revised Class E airspace established upward from 700 feet (ft.) and 1,200 ft. above the surface at Atqasuk Edward Burnell Sr. Memorial Airport, AK.
Revision of Class E Airspace; Big Lake, AK
Document Number: E6-8283
Type: Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Big Lake, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) along with one amended SIAP. This rule results in revised Class E airspace established upward from 700 feet (ft.) above the surface at Big Lake, AK.
Proposed Revision of Class E Airspace; Willow, AK
Document Number: E6-8281
Type: Proposed Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Willow, AK. Two Standard Instrument Approach Procedures (SIAPs) along with one Standard Instrument Departure (SID) and a published departure procedure (DP) are being developed for the Willow Airport. 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 Willow, AK.
Establishment of VOR Federal Airway V-623; NJ and NY
Document Number: E6-8280
Type: Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
This action establishes VOR Federal Airway V-623 between the Sparta, NJ, Very High Frequency Omnidirectional Range Tactical Air Navigation (VORTAC) and the Carmel, NY, Very High Frequency Omnidirectional Range/Distance Measuring Equipment (VOR/DME). The FAA is taking this action to enhance the management of aircraft transiting from the New England area to airports in the Newark, NJ, area.
Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes
Document Number: 06-55518
Type: Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
Notice of Opportunity for Public Comment on Surplus Property Release at the Brunswick Golden Isles Airport, Brunswick, GA
Document Number: 06-4939
Type: Notice
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
Under the provisions of Title 49, U.S.C. 47153(c), notice is being given that the FAA is considering a request from Glynn County to waive the requirement that approximately 18.50 acres of surplus property, located at the Brunswick Golden Isles Airport, be used for aeronautical purposes.
Notice of Opportunity for Public Comment on Surplus Property Release at McKinnon St. Simons Island Airport, Brunswick, GA
Document Number: 06-4938
Type: Notice
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
Under the provisions of Title 49, U.S.C. 47153(c), notice is being given that the FAA is considering a request from Glynn County to waive the requirement that approximately 3.17 acres of surplus property, located at the McKinnon St. Simons Island Airport, be used for aeronautical purposes.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU Airplanes; and Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 190-100 LR, -100 STD, and -100 IGW Airplanes
Document Number: 06-4909
Type: Rule
Date: 2006-05-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all EMBRAER Model ERJ 170 and Model ERJ 190 airplanes. This AD requires revising the Limitations section of the airplane flight manual to prohibit the flightcrew from moving the throttle into the forward thrust range immediately after applying the thrust reverser. This AD results from a report that, during landing, the thrust reverser may not re-stow completely if the throttle lever is moved into the forward thrust range immediately after the thrust reverser is applied. We are issuing this AD to prevent the flightcrew from performing a takeoff with a partially deployed thrust reverser, which could result in reduced controllability of the airplane.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: E6-8199
Type: Notice
Date: 2006-05-26
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 2006-24881 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: E6-8197
Type: Notice
Date: 2006-05-26
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 2006-24894 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: E6-8190
Type: Notice
Date: 2006-05-26
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 2006-24879 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: E6-8189
Type: Notice
Date: 2006-05-26
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 2006-24882 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: E6-8188
Type: Notice
Date: 2006-05-26
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 2006-24880 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: E6-8187
Type: Notice
Date: 2006-05-26
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 2006-24883 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.
Denial of Motor Vehicle Defect Petition
Document Number: E6-8151
Type: Notice
Date: 2006-05-26
Agency: National Highway Traffic Safety Administration, Department of Transportation
This notice sets forth the reasons for the denial of a petition submitted by Mr. Brad Lamb to NHTSA's Office of Defects Investigation (ODI), received December 2, 2005, under 49 U.S.C. 30162, requesting that the agency commence a proceeding to determine the existence of a defect related to motor vehicle safety with respect to the parking brakes on: (1) Model year (MY) 1999-2003 Chevrolet Silverado and GMC Sierra pickup trucks; (2) MY 2002-2003 Cadillac Escalade and Chevrolet Avalanche sport-utility vehicles (SUV); and (3) MY 2000-2003 Chevrolet Suburban/Tahoe and GMC Yukon SUV. After a review of the petition and other information, NHTSA has concluded that further expenditure of the agency's investigative resources on the issues raised by the petition does not appear to be warranted. The agency accordingly has denied the petition. The petition is hereinafter identified as DP05-009.
Airworthiness Directives; Boeing Model 777-200, -300, and -300ER Series Airplanes
Document Number: E6-8123
Type: Proposed Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 777-200, -300, and -300ER series airplanes. This proposed AD would require replacement of the gimbal plates of the left and right outboard trailing edge flaps with improved gimbal plates and other specified actions. This proposed AD results from a broken pivot link found on the inboard support for the outboard trailing edge flap. We are proposing this AD to prevent disconnection of the drive arm from its drive gimbal, due to a broken pivot link on an outboard flap support, which could result in unexpected roll of the airplane and loss of control of the airplane.
Airworthiness Directives; Airbus Model A330 Airplanes and Model A340-200 and -300 Series Airplanes
Document Number: E6-8122
Type: Proposed Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain Airbus Model A330 airplanes and Model A340-200 and -300 series airplanes. The original NPRM would have required repetitive detailed inspections for cracking in the aft web of support rib 6 between certain bottom skin stringers on both wings; high frequency eddy current inspections for cracking of the attachment holes of the fuel pipes, and repair if necessary. The original NPRM also would have provided for an optional modification, which would extend a certain inspection threshold. The original NPRM resulted from a report of significant cracking found in the aft web of support rib 6 on both wings. This action revises the original NPRM by mandating, for certain airplanes, a new modification of support rib 6 on both wings, which would end the repetitive inspection requirement. This action also reduces the applicability in the original NPRM. We are proposing this supplemental NPRM to prevent cracking in the aft web of support rib 6, which could result in overloading of adjacent ribs and the surrounding wing structure and consequent reduced structural integrity of the wing.
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: E6-8121
Type: Proposed Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain EMBRAER Model EMB-135 and -145 series airplanes. The original NPRM would have required determining the torque values of the screws that attach the seat tracks to the airplane, and corrective action if necessary. The original NPRM resulted from a report of undertorqued screws. This action revises the original NPRM by referring to revised service information and expanding the applicability. We are proposing this supplemental NPRM 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 737-300, -400, -500, -600, -700, -700C, -800, and -900 Series Airplanes
Document Number: E6-8120
Type: Proposed Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 737-300, -400, -500, -600, - 700, -700C, -800, and -900 series airplanes. The original NPRM would have required modifying the wiring for the master dim and test system. For certain airplanes, the original NPRM also proposed to require related concurrent actions as necessary. The original NPRM resulted from a report that the master dim and test system circuit does not have wiring separation of the test ground signal for redundant equipment in the flight compartment. This action revises the original NPRM by adding a new concurrent action for certain airplanes, extending the compliance time, and removing certain airplanes from concurrent requirements. We are proposing this supplemental NPRM to prevent a single fault failure in flight from simulating a test condition and showing test patterns instead of the selected radio frequencies on the communications panels, which could inhibit communication between the flightcrew and the control tower, affecting the continued safe flight of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ and EMB-145XR Airplanes
Document Number: E6-8117
Type: Proposed Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
This document revises an earlier supplemental notice of proposed rulemaking (NPRM), applicable to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ and Model EMB-145XR airplanes. The first supplemental NPRM would have required, for all airplanes, installation of an additional indication device to the clear-ice indication system. For certain airplanes, the first supplemental NPRM would also have required replacing the existing clear-ice indication lamp with a new, improved lamp. For certain other airplanes, the first supplemental NPRM would also have required modifying certain electrical connections to add an indication device to the clear-ice indication system; removing a certain placard; and re- activating the clear-ice additional indicator lamp. This new action revises the first supplemental NPRM by adding airplanes to the applicability. The actions specified by this new proposed supplemental NPRM are intended to prevent undetected build-up of clear ice on the wing surfaces, which could lead to reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Boeing Model 737-300, -400, -500, -600, -700, -700C, -800, and -900, and 747-400 Series Airplanes; and Model 757, 767, and 777 Airplanes
Document Number: E6-8115
Type: Proposed Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
This document revises an earlier proposed airworthiness directive (AD), applicable to certain Boeing Model 737-300, -400, -500, -600, -700, -700C, -800, and -900, and 747-400 series airplanes; and Model 757, 767, and 777 airplanes. The original NPRM would have required modifying the static inverter by relocating resistor R170 of the static inverter bridge assembly. This new action revises the original NPRM by adding a new requirement for modifying the static inverter by replacing resistor R170 with a new resistor and relocating the new resistor. The actions proposed by this supplemental NPRM are intended to prevent a standby static inverter from overheating, which could result in smoke in the flight deck and cabin and loss of the electrical standby power system. This action is intended to address the identified unsafe condition.
BNSF Railway Company-Temporary Trackage Rights Exemption-Union Pacific Railroad Company
Document Number: E6-8038
Type: Notice
Date: 2006-05-26
Agency: Surface Transportation Board, Department of Transportation
Environmental Impact Statement; Humboldt County, CA
Document Number: 06-4876
Type: Notice
Date: 2006-05-26
Agency: Federal Highway Administration, Department of Transportation
The FHWA is republishing this notice to advise the public that an Environmental Impact Statement (EIS) will be prepared for the proposed highway project along U.S. Highway (Highway) 101 in Humboldt County, in the Cities of Eureka and Arcata, and the unincorporated area between the two cities, California. The original Notice of Intent (NOI) was published in the Federal Register on August 31, 2001, (Volume 66, Number 170, Pages 46061 & 46062). The NOI is being republished due to project changes of adding roadway rehabilitation work and new alternatives to the proposed project.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 06-4847
Type: Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD requires revising the Airworthiness Limitations section of the Instructions for Continuing Airworthiness of the Maintenance Requirements Manual to include revised threshold and repeat inspection intervals for the cargo door skin cut-out. This AD results from a report that a crack was discovered at the lower forward corner of a cargo door skin cut-out during fatigue testing. We are issuing this AD to detect and correct cracking in the lower forward corner of the cargo door skin cut-out, which could result in reduced structural integrity of the airplane.
Airworthiness Directives; Boeing Model 767 Airplanes
Document Number: 06-4846
Type: Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 767 airplanes. This AD requires repetitive measurements of the rudder and elevator freeplay, repetitive lubrication of rudder and elevator components, and related investigative/corrective actions if necessary. This AD results from reports of freeplay-induced vibration of the rudder and the elevator. The potential for vibration of the control surface should be avoided because the point of transition from vibration to divergent flutter is unknown. We are issuing this AD to prevent excessive vibration of the airframe during flight, which could result in loss of control of the airplane.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
Document Number: 06-4845
Type: Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 777-200 and -300 series airplanes. This AD requires replacing the battery packs of the emergency power assist system (EPAS) of the left and right non-overwing exit doors with new or modified battery packs. This AD results from intermittent failures of the EPAS battery pack found during testing, which are due to switch contamination, cam alignment problems, and inadequate self-test capability. We are issuing this AD to prevent failure of the EPAS, which could result in the inability to open the exit door during an emergency evacuation.
Airworthiness Directives; Boeing Model 757 Airplanes
Document Number: 06-4844
Type: Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 757 series airplanes. That AD currently requires revising the Airworthiness Limitations section of the maintenance manual (757 Airworthiness Limitations Instructions (ALI)) to incorporate certain inspections and compliance times to detect fatigue cracking of principal structural elements (PSEs). This new AD requires incorporating a new revision to the Airworthiness Limitations section of the Instructions of Continued Airworthiness to mandate certain repetitive inspections for fatigue cracking of PSEs, and adds airplanes to the applicability in the existing AD. This AD results from a new revision to the ALI. We are issuing this AD to ensure that fatigue cracking of various PSEs is detected and corrected; such fatigue cracking could adversely affect the structural integrity of these airplanes.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes
Document Number: 06-4843
Type: Rule
Date: 2006-05-26
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-120, -120ER, -120FC, -120QC, and -120RT airplanes. This AD requires replacing the de-icing system ejector flow control valves with new, improved control valves having hermetically sealed switches; and rewiring applicable connectors. This AD results from a fuel system review conducted by the manufacturer. We are issuing this AD to prevent a potential source of ignition near a fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Voluntary Disclosure Reporting Program
Document Number: E6-8078
Type: Proposed Rule
Date: 2006-05-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is proposing that information provided to the agency from a Voluntary Disclosure Reporting Program (VDRP) be designated by an FAA order as protected from public disclosure in accordance with the provisions of 14 CFR part 193. Under 49 U.S.C. 40123, the FAA is required to protect the information from disclosure to the public, including disclosure under the Freedom of Information Act (5 U.S.C. 552) or other laws, following issuance of such order. The designation is intended to encourage participation in the VDRP.
Qualification of Drivers; Exemption Applications; Vision
Document Number: E6-8076
Type: Notice
Date: 2006-05-25
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
FMCSA announces its decision to exempt 16 individuals from the vision requirement in the Federal Motor Carrier Safety Regulations (FMCSRs). The exemptions will enable these individuals to operate commercial motor vehicles (CMVs) in interstate commerce without meeting the prescribed vision standard. The Agency has concluded that granting these exemptions will provide a level of safety that is equivalent to, or greater than, the level of safety maintained without the exemptions for these CMV drivers.
Hazardous Materials: Preemption Determinations; Procedural Regulations
Document Number: E6-8064
Type: Rule
Date: 2006-05-25
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
The Pipeline and Hazardous Materials Safety Administration is revising its procedural regulations for issuing administrative determinations as to whether Federal hazardous material transportation law preempts a State, local, or Indian tribe requirement and for issuing waivers of preemption.
Aviation Proceedings, Agreements Filed the Week Ending May 5, 2006
Document Number: E6-8044
Type: Notice
Date: 2006-05-25
Agency: Office of the Secretary, Department of Transportation
Environmental Impact Statement: Oconto and Marinette Counties, WI
Document Number: E6-8012
Type: Notice
Date: 2006-05-25
Agency: Federal Highway Administration, Department of Transportation
The FHWA and WisDOT are issuing this notice to advise the public that an Environmental Impact Statement (EIS) will be prepared for proposed transportation improvements in the United States Highway (US) 51 corridor in the city of Madison, Dane County, Wisconsin generally between US 12/18 (South Beltline Highway) and State Trunk Highway (STH) 19. The EIS is being prepared in conformance with 40 CFR 1500 and FHWA regulations.
Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes
Document Number: E6-8011
Type: Proposed Rule
Date: 2006-05-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all McDonnell Douglas Model MD-90-30 airplanes. This proposed AD would require installing a clamp, bonding jumper assembly, and attaching hardware to the refueling manifold in the right wing refueling station area. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent arcing on the in-tank side of the fueling valve during a lightning strike, which could result in an ignition source that could ignite fuel vapor and cause a fuel tank explosion.
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