Department of Transportation 2007 – Federal Register Recent Federal Regulation Documents
Results 1,851 - 1,900 of 3,086
Hours of Service (HOS) of Drivers; Renewal of American Pyrotechnics Association (APA) Exemption From the 14-Hour Rule during Independence Day Celebrations
FMCSA announces its decision to renew the American Pyrotechnics Association (APA) exemption from FMCSA's regulation that drivers of commercial motor vehicles (CMVs) may not drive after the 14th hour of coming on duty. The exemption for 70 motor carriers and approximately 3,000 drivers is applicable for a period beginning 7 days prior to and 2 days immediately following Independence Day in 2007 and 2008. Drivers who operate CMVs in conjunction with staging fireworks shows celebrating Independence Day will be allowed to exclude off-duty and sleeper-berth time of any length from the calculation of the 14 hours. These drivers will not be allowed to drive after accumulating a total of 14 hours of on-duty time, following 10 consecutive hours off duty, and will continue to be subject to the 11- hour driving time limit, and the 60- and 70-hour on-duty limits. The terms and conditions of the current exemption will remain in place for a second two-year period. FMCSA believes that with the terms and conditions in place, APA will maintain a level of safety that is equivalent to, or greater than, the level of safety that would be obtained by complying with the regulation.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
The FAA is superseding an existing airworthiness directive (AD) that applies to all Model 737-100, -200, -300, -400, and -500 series airplanes. The existing AD currently requires repetitive detailed inspections for damage of the electrical wire and sleeve that run through a conduit in the fuel tank to the fuel boost pump, and related investigative and corrective actions; as applicable. This new AD removes certain inspection requirements. This new AD adds repetitive detailed inspections for damage of the electrical wire and sleeve that run to the fuel boost pump through a conduit in the fuel tank, and arcing damage of the conduit and signs of fuel leakage into the conduit; replacement of the sleeve with a new, smaller-diameter sleeve; and related investigative and corrective actions, as applicable. This AD also adds airplanes to the applicability. Accomplishment of the initial new inspection and the sleeve installation terminates the requirements of the existing AD. This new AD results from a report of a fuel tank explosion on a Model 727-200F airplane on the ground, and a report of chafed wires and a damaged power cable sleeve of a fuel boost pump discovered during an inspection on a Model 737-300 airplane. We are issuing this AD to detect and correct chafing of the fuel boost pump electrical wiring and leakage of fuel into the conduit, and to prevent electrical arcing between the wiring and the surrounding conduit, which could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank.
Airworthiness Directives; Boeing Model 727 Airplanes
The FAA is superseding an existing airworthiness directive (AD) that applies to all Boeing Model 727 airplanes. The existing AD requires a boost pump dry bay inspection to detect leakage of fuel through an arced-through conduit, and corrective action as necessary. The existing AD also requires repetitive inspections of the in-tank fuel boost pump wiring to detect chafing of the wire insulation, evidence of electrical arcing, or arc-through of the conduit wall, and applicable corrective action; and installation of sleeving over the in- tank fuel boost pump wires as a method to protect the wiring from chafing. This new AD removes certain inspection requirements from the existing AD. This new AD adds new repetitive inspections for damage of the electrical wire and sleeve that run to the fuel boost pump through a conduit in the fuel tank, and arcing damage of the conduit and signs of fuel leakage into the conduit; applicable investigative and corrective actions; and a new repetitive engine fuel suction feed operational test. Initiation of the new inspections terminates the requirements of the existing AD. This AD results from reports of a fuel tank explosion on a Model 727-200F airplane on the ground; and of chafed wires and a damaged power cable sleeve of a fuel boost pump that were discovered during an inspection required by an existing AD on a Model 737-300 airplane. We are issuing this AD to detect and correct chafing of the fuel boost pump electrical wiring and leakage of fuel into the conduit, and to prevent electrical arcing between the wiring and the surrounding conduit, which could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank.
Proposed Revision of Class E Airspace; Ruby, AK
This action proposes to revise Class E airspace at Ruby, AK. Two Standard Instrument Approach Procedures (SIAPs) are being amended for the Ruby Airport at Ruby, AK. Adoption of this proposal would result in revision of existing Class E airspace upward, from 700 feet (ft.) and 1,200 ft. above the surface, at the Ruby Airport, Ruby, AK.
Proposed Establishment of Low Altitude Area Navigation Route T-209; GA
This action proposes to establish a low altitude Global Positioning System (GPS)/Global Navigation Satellite System (GNSS) area navigation (RNAV) route, designatedT-209, in the vicinity of Augusta, GA. The FAA is proposing this action to enhance the safe and efficient use of the navigable airspace. The proposed route would reduce air traffic controller workload and provide a nonradar route that ensures clearance from the Bulldog A Military Operations Area (MOA).
Proposed Revision of Class E Airspace; Kotzebue, AK
This action proposes to revise Class E airspace at Kotzebue, AK. Eight (8) Standard Instrument Approach Procedures (SIAPs) are being amended for the Ralph Wien Memorial Airport at Kotzebue, AK. A Departure Procedure (DP) is also being amended. Adoption of this proposal would result in revision of existing Class E airspace upward from the surface, from 700 feet (ft.) and 1,200 ft. above the surface, at the Ralph Wien Memorial Airport, Kotzebue, AK.
Proposed Revision of Class E Airspace; Fort Yukon, AK
This action proposes to revise Class E airspace at Fort Yukon, AK. One Standard Instrument Approach Procedure (SIAP) is being amended and three new SIAPs are being developed for the Fort Yukon Airport. A Departure Procedure (DP) and a Direction Finding (DF) procedure (used by Flight Service Station personnel) is also being amended. Adoption of this proposal would result in revision of existing Class E airspace upward from the surface, from 700 feet (ft.) and 1,200 ft. above the surface, at Fort Yukon Airport, Fort Yukon, AK.
Proposed Revision of Class E Airspace; Noatak, AK
This action proposes to revise Class E airspace at Noatak, AK. One Standard Instrument Approach Procedure (SIAP) is being amended for the Noatak Airport at Noatak, AK. A Departure Procedure (DP) is also being amended. Adoption of this proposal would result in revision of existing Class E airspace upward, from 700 feet (ft.) and 1,200 ft. above the surface, at the Noatak Airport, Noatak, AK.
Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines
The FAA is superseding an existing airworthiness directive (AD) for Turbomeca Arrius 2F turboshaft engines. That AD currently requires removing from service certain serial number (SN) fuel control units (FCUs) or replacing the constant delta pressure (delta P) diaphragm in those FCUs. This AD requires replacing all FCUs not incorporating modification Tf 55 with FCUs that incorporate modification Tf 55. This AD results from the European Aviation Safety Agency (EASA) and Turbomeca expanding the applicability to the full population of FCUs installed on Arrius 2F turboshaft engines. FCUs not incorporating modification Tf 55 are susceptible to having an improperly assembled constant delta P diaphragm. We are issuing this AD to prevent an uncommanded engine in-flight shutdown on a single-engine helicopter, resulting in a forced autorotation landing or an accident.
Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction
The FAA is correcting airworthiness directive (AD) 2006-24-08. That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines. We published that AD in the Federal Register on December 4, 2006 (71 FR 70284). The fuel manifold part number (P/N) 3025267-01 listed in paragraph (c) is incorrect. This document corrects that P/N. In all other respects, the original document remains the same.
Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Dornier Luftfahrt GmbH Model 228 Series Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; British Aerospace Regional Aircraft Model HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 Airplanes
We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
RTCA Government/Industry Air Traffic Management Advisory Committee
The FAA is issuing this notice to advise the public of a meeting of RTCA Government/Industry Air Traffic Management Advisory Committee.
Proposed Establishment of Class E Airspace; Centreville, AL
This notice proposed to establish Class E airspace at Centreville, AL. An Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) Runway (RWY) 10 has been developed for Bibb County Airport. As a result, controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP and for Instrument Flight Rules (IFR) operations at Bibb County Airport. The operating status of the airport will change from Visual Flight Rules (VFR) to include IFR operations concurrent with the publication of the SIAP.
Office of Hazardous Materials Safety; Notice of Application for Special Permits
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR part 107, subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. Each mode of transportation for which a particular special permit is requested is indicated by a number in the ``Nature of Application'' portion of the table below as follows: 1Motor vehicle, 2Rail freight, 3Cargo vessel, 4Cargo aircraft only, 5Passenger-carrying aircraft.
Office of Hazardous Materials Safety; Notice of Applications for Modification of Special Permit
In accordance with the procedures governing the application for, and the processing of, special permits from the Department of Transportation's Hazardous Material Regulations (49 CFR part 107, subpart B), notice is hereby given that the Office of Hazardous Materials Safety has received the application described herein. This notice is is abbreviated to expedite docketing and public notice. Because the sections affected, modes of transportation, and the nature of application have been shown in earlier Federal Register publications, they are not repeated here. Request of modifications of special permits (e.g., to provide for additional hazardous materials, packaging design changes, additional mode of transportation, etc.) are described in footnotes to the application number. Application numbers with the suffix ``M'' denote a modification request. These applications have been separated from the new application for special permits to facilitate processing.
Proposed Establishment of Class E Airspace; Vero Beach, FL
This notice proposes to establish Class E2 airspace at Vero Beach, FL. As a result of an evaluation, it has been determined Class E Airspace Designated as Surface Areas should be established for Vero Beach Municipal Airport. Miami Air Route Traffic Control Center has communications capabilities and weather observation reporting when the Vero Beach tower is closed. Therefore, the airport will meet criteria for Class E2 airspace. Class E2 surface area airspace is required when the control tower is closed to contain Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action would establish Class E2 airspace extending upward from the surface to and including 2,500 feet MSL within a 4.2- mile radius of the airport and within 3.2 miles each side of the 261[deg] bearing from the Vero Beach Nondirectional Radio Beacon (NDB) extending from the 4.2 mile radius of the Vero Beach Municipal Airport to 7 miles west of the NDB.
Public Notice for Waiver of Aeronautical Land-Use Assurance Rickenbacker International Airport Columbus, OH
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the airport from aeronautical use to non-aeronautical use and to authorize the release of 188.653 acres of vacant airport property previously used for agricultural purposes for the proposed development of bulk warehouse/distribution facilities as a component of the Rickenbacker Global Logistics Park. The land was acquired by the Rickenbacker Port Authority through three Quitclaim Deeds from the United States of American dated March 30, 1984, September 22, 2004 (amended and restated August 26, 2005) and May 16, 2005. There are no impacts to the airport by allowing the airport to dispose of the property. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The CRAA will receive $4,245,000 for the parcel. 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.
Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters
This document proposes adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC 130 B4 helicopters, with certain twist grip assemblies installed. This proposal would require inspecting the pilot and co-pilot collective levers for proper bonding between the twist grip drive tubes and the control pinions and if debonding is present, replacing the collective levers before further flight. This proposal is prompted by one incident in which the engine remained at idle speed although the twist grip had been turned to the flight position. The actions specified by this proposed AD are intended to detect debonding between the twist grip drive tubes and the control pinions on the pilot and co-pilot collective levers to prevent loss of cockpit throttle control of the engine, and subsequent loss of control of the helicopter.
Airworthiness Directives; Pratt & Whitney (PW) PW4164, PW4168, and PW4168A Turbofan Engines
The FAA proposes to adopt a new airworthiness directive (AD) for PW PW4164, PW4168, and PW4168A turbofan engines with certain low pressure turbine (LPT) stage 4 disks, part number (P/N) 51N404, installed. This proposed AD would require removing certain LPT stage 4 disks, listed by serial number at the next piece-part exposure or within 7,500 cycles-since-new (CSN), whichever occurs first. This proposed AD results from a report of improperly manufactured LPT stage 4 disks. We are proposing this AD to prevent an uncontained engine failure due to low-cycle fatigue (LCF), which could result in damage to the airplane.
Airworthiness Directives; Eurocopter France Model EC130 B4 Helicopters
This amendment proposes adopting a new airworthiness directive (AD) for Eurocopter France (ECF) Model EC130 B4 helicopters. This proposal would require, within 100 hours time-in-service (TIS), modifying and testing the wiring of the battery overheat sensing circuit. This proposal is prompted by a malfunction in the battery overheat sensing circuit found during a scheduled inspection. The actions specified by this proposed AD are intended to correct the connection of the thermal switch to the cockpit indicator light, to notify the flight crew of an overheated battery, and to prevent a thermal runaway of the battery, an in-flight fire, and subsequent loss of control of the helicopter.
Office of Small and Disadvantaged Business Utilization; Solicitation of Applications for Regional Small Business Transportation Resource Centers (SBTRCs) Fiscal Year (FY) 2007, Grant Opportunity
OSDBU announces that it has published an opportunity to apply for the FY 2007 Small Business Transportation Business Resource Center funding on the grants.gov Web site (https://www.grants.gov). Section 4134 of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: OSDBU is responsible for the implementation and execution of the Department of Transportation (DOT) activities on behalf of small businesses in accordance with Section 8, 15 and 31 of the Small Business Act (SBA), as amended. The OSDBU also administers the provisions of Title 49, the Minority Resource Center (MRC) which includes the duties of advocacy, outreach and financial services on behalf of small and disadvantaged business and those certified under CFR 49 parts 23 and or 26 as Disadvantaged Business Enterprises (DBE). This request solicits competitive proposals from business centered community-based organizations, transportation-related trade associations, colleges and universities, community colleges or chambers of commerce for participation in OSDBU's Small Business Transportation Resource Centers (SBTRC) under the Minority Resource Center (MRC) program. OSDBU will enter into Cooperative Agreements with these organizations to outreach to the small business community in their designated region and provide financial and technical assistance, business training programs such as, business assessment, management training, counseling, technical assistance, marketing and outreach, and the dissemination of information, to encourage and assist small businesses to become better prepared to compete for, obtain, and manage DOT funded transportation-related contracts and subcontracts at the Federal, State and local levels. Eligible applicants must be registered with the Internal Revenue Service as 501 C(6) or 501 C(3) tax-exempt organizations. To apply for funding, applicants must be registered with grants.gov. Registration with grants.gov may take two to five days before the system will allow you to apply for grants using the grants.gov Web site https://www.grants.gov/applicants/get registered.jsp). Submit application in accordance with the instructions provided. Applications for grant funding must be submitted electronically to OSDBU through the grants.gov Web site.
Railroad Cost of Capital-2006
The Board is instituting a proceeding to determine the railroad industry's cost of capital for 2006. The decision solicits comments on: (1) The railroads' 2006 current cost of debt capital; (2) the railroads' 2006 current cost of preferred stock equity capital (if any); (3) the railroads' 2006 cost of common stock equity capital; and (4) the 2006 capital structure mix of the railroad industry on a market value basis.
Notice and Request for Comments
As required by the Paperwork Reduction Act of 1995, 44 U.S.C. 3501 et seq. (PRA), the Surface Transportation Board (STB or Board) gives notice of its intent to seek from the Office of Management and Budget (OMB) an approval for the currently existing collection of Waybill Sample data. This information collection is described in detail below. Comments are requested concerning: (1) The accuracy of the Board's burden estimates; (2) ways to enhance the quality, utility, and clarity of the information collected; (3) ways to minimize the burden of the collection of information on the respondents, including the use of automated collection techniques or other forms of information technology, when appropriate; and (4) whether this collection of information is necessary for the proper performance of the functions of the Board, including whether the collection has practical utility. Submitted comments will be summarized and included in the Board's request for OMB approval.
Petition for Exemption From the Federal Motor Vehicle Motor Theft Prevention Standard; MAZDA
This document grants in full the petition of Mazda Motor Corporation, (Mazda) for an exemption in accordance with Sec. 543.9(c)(2) of 49 CFR Part 543, Exemption from the Theft Prevention Standard, for the Mazda 5 vehicle line beginning with model year (MY) 2009. This petition is granted because the agency has determined that the antitheft device to be placed on the line as standard equipment is likely to be as effective in reducing and deterring motor vehicle theft as compliance with the parts-marking requirements of the Theft Prevention Standard.
Requested Administrative Waiver of the Coastwise Trade Laws
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 MARAD-2007-28175 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
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 MARAD-2007-28176 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
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 MARAD-2007-28167 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.
Ninth Meeting: RTCA Special Committee 206/EUROCAE WG 76 Plenary
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 206: Aeronautical Information Services Data Link.
Airworthiness Directives; British Aerospace Regional Aircraft Model Jetstream HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Pacific Aerospace Limited, Model 750XL Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Qualification of Drivers; Exemption Applications; Vision
FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 22 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemptions will provide a level of safety that will be equivalent to, or greater than, the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.
Relocation of DOT's Docket Operations Facility and Equipment and Temporary Docket Office Closure for All DOT Agencies, and Other Users, Including the Transportation Security Administration and the United States Coast Guard
This notice announces two service disruptions relating to the relocation of the U.S. Department of Transportation (DOT) Docket Operations Facility, which manages the Docket Management System (DMS) containing the public dockets for all agencies of the Department of Transportation, except the Surface Transportation Board. DOT's Docket Operations facility is moving to 1200 New Jersey Avenue, SE., Washington, DC 20590 and will be located on the West Building Ground Floor, Room W12-140. Hours for the new facility will continue to be 9 a.m. to 5 p.m., Monday through Friday, excluding legal holidays. The Docket Operations telephone number will continue to be (202) 366-9826. 1. To prepare for the relocation to the new facility, the Docket Operations office will be closed to the public on Friday, May 25, 2007, through Tuesday, May 29, 2007. The office will reopen to the public on Wednesday, May 30, 2007 at the new facility. 2. To move the computers that host the electronic dockets, the DMS will be unavailable for use from Wednesday, June 13, 2007, through Sunday, June 17, 2007. The electronic docket will again be available to users starting on June 18, 2007.
Airworthiness Directives; British Aerospace Regional Aircraft Jetstream Model 3201 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Pipeline Safety: Protecting Unusually Sensitive Areas From Rural Low-Stress Hazardous Liquid Pipelines
In this supplemental notice of proposed rulemaking (SNPRM) PHMSA is modifying its pending proposal for regulating rural low-stress hazardous liquid pipelines within a prescribed buffer of an ``unusually sensitive area'' (USA). This modification addresses new requirements in the Pipeline Inspection, Protection, Enforcement, and Safety Act of 2006 (PIPES Act). We propose to apply all Federal hazardous liquid pipeline safety regulations to these pipelines instead of the narrower, threat-focused set of requirements we originally proposed to apply to these pipelines. This action will help protect USAs from the potential adverse impacts of releases from low-stress hazardous liquid pipelines in rural areas.
Airworthiness Directives; Diamond Aircraft Industries GmbH Model DA 40 and DA 40F Airplanes
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Human Space Flight Requirements for Crew and Space Flight Participants
This notice announces the Office of Management and Budget's (OMB) approval of the information collection requirement in the final rule published on December 15, 2006. The sections of the final rule pending approval of this information collection request are effective upon publication of this notice.
Petitions for Exemption; Summary of Petitions Received
This notice contains a summary of a certain petition 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.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145LR, -145XR, and -145MP Airplanes; and Model EMB-135BJ and -135LR Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-145LR, -145XR, and -145MP airplanes; and Model EMB-135BJ and -135LR airplanes. This AD requires replacing the electrical bonding clamps inside the fuel tanks and adjacent areas. This AD results from a report of the failure of a fitting clamp of an electrical bonding cable for the fuel tubing. We are issuing this AD to prevent loss of bonding protection in the interior of the fuel tanks or adjacent areas, and a consequent potential source of ignition in a fuel tank and possible fire or explosion.
Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes
The FAA is adopting a new airworthiness directive (AD) to supersede AD 2006-06-06, which applies to certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. AD 2006-06-06 currently requires you to incorporate information into the applicable section of the Airplane Flight Manual (AFM) and Pilot's Operating Handbook (POH) and requires you to install placards. Since we issued AD 2006-06-06, Cessna issued new S1 Known Icing Equipment AFM supplements and developed a low airspeed awareness system. Consequently, this AD requires you to incorporate the applicable AFM supplement revision and temporarily retain the requirements of AD 2006-06-06 until the above revisions are incorporated. One of the AFM requirements is the installation of a functional low airspeed awareness system to operate the airplane in known icing conditions. We are issuing this AD to assure that the pilot has enough information and the necessary equipment to prevent loss of control of the airplane while in-flight during icing conditions.
Airworthiness Directives; Boeing Model 747-400 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-400 series airplanes. This AD requires repetitive inspections for any crack in the upper deck floor beam at station 400, which include inspecting the floor beam web and chords, certain fastener holes at the intersection of the floor beam and frame on both sides of the airplane, and certain floor panel attachment fastener holes at the floor beam upper chords. This AD also requires corrective action if necessary. This AD results from several reports indicating that fatigue cracking was found in upper deck floor beams made from 7000 series aluminum alloy. We are issuing this AD to detect and correct cracking in the upper deck floor beam at station 400, which could extend and sever the floor beam. A severed floor beam could result in loss of controllability and rapid decompression of the airplane.
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