Department of Transportation May 2015 – Federal Register Recent Federal Regulation Documents
Results 201 - 228 of 228
Airworthiness Directives; Airbus Helicopters (Type Certificate Previously Held by Eurocopter France)
We are adopting a new airworthiness directive (AD) for Airbus Model EC225LP helicopters. This AD requires repetitive visual and tap test inspections of each main rotor blade (blade) leading edge stainless steel protective strip (strip) for a crack, cut, or blind or open debonding (debonding), and taking approved corrective measures. If there is a crack or if there is debonding that exceeds acceptable limits, this AD requires, before further flight, repairing or replacing the blade with an airworthy part. This AD was prompted by suspected water seepage through a crack in the blade strip resulting in significant debonding. The actions of this AD are intended to prevent loss of the blade strip, excessive vibrations induced by blade weight imbalance, and subsequent loss of control of the helicopter.
Air Carrier Contract Maintenance Requirements; Correction
The FAA is correcting a final rule published on March 4, 2015 (80 FR 11537). In that rule, the FAA amended its maintenance regulations for domestic, flag, and supplemental operations, and for commuter and on-demand operations for aircraft type certificated with a passenger seating configuration of 10 seats or more (excluding any pilot seat). The FAA originally proposed to make the effective date of the rule one year after its publication date to give affected operators time to come into compliance with the new requirements, and to allow the FAA time to review information submitted by the operators under the rule. However, in the final rule, the FAA inadvertently overlooked the proposed one-year compliance time, and included an effective date of 60 days after publication. This document corrects the effective date of that document.
Decision That Nonconforming Model Year 2010 European Market Ferrari California Passenger Cars Are Eligible for Importation
This document announces a decision by the National Highway Traffic Safety Administration that certain Model Year (MY) 2010 Ferrari California passenger cars (PCs) that were not originally manufactured to comply with all applicable Federal Motor Vehicle Safety Standards (FMVSS) are eligible for importation into the United States because they are substantially similar to vehicles originally manufactured for importation into and sale in the United States that were certified by their manufacturer as complying with the safety standards (the U.S. certified version of the MY 2010 Ferrari California PC), and they are capable of being readily altered to conform to the standards.
Continental Tire the Americas, LLC, Receipt of Petition for Decision of Inconsequential Noncompliance
Continental Tire the Americas, LLC, (CTA), has determined that certain Continental Tire brand TKC80 motorcycle replacement tires do not fully comply with paragraph S6.5(c) of Federal Motor Vehicle Safety Standard (FMVSS) No. 119, New Pneumatic Radial Tires for motor vehicles with a GVWR of more than 4,536 Kilograms (10,000 pounds) and Motorcycles. CTA has filed an appropriate report dated February 18, 2015, pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports.
Airworthiness Directives; Fokker Services B.V. Airplanes
We propose to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F.27 Mark 200, 300, 400, 500, 600, and 700 airplanes. This proposed AD was prompted by a design review, which revealed that no controlled bonding provisions are present on a number of critical locations inside the fuel tank or connected to the fuel tank wall; and no anti-spray cover is installed on the fuel shut-off valve (FSOV) in both wings. This proposed AD would require installing additional bonding provisions in the fuel tank, installing an anti- spray cover on the FSOV, and revising the airplane maintenance program by incorporating fuel airworthiness limitation items and critical design configuration control limitations. We are proposing this AD to prevent an ignition source in the fuel tank vapor space, which could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Dassault Aviation Airplanes
We propose to adopt a new airworthiness directive (AD) for all Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. This proposed AD was prompted by reports of defective fire extinguisher tubes. It was determined the defects were caused by corrosion. This proposed AD would require repetitive general visual inspections of the fire extinguisher tubes for cracking and corrosion, and replacement of any cracked tube with a serviceable tube, if necessary. We are proposing this AD to detect and correct cracking and corrosion in the fire extinguisher tubes, which could impact the capability to extinguish an engine fire, and possibly result in damage to the airplane and injury to the passengers.
Airworthiness Directives; Airbus Airplanes
We propose to supersede Airworthiness Directive (AD) 2011-24- 05, for certain Airbus Model A330-201, -202, -203, -223, -243, -301, - 302, -303, -321, -322, -323, -341, -342, and -343 airplanes; and Model A340-200 and -300 series airplanes. AD 2011-24-05 currently requires repetitive inspections for cracking of the hole(s) of the horizontal flange of the keel beam, and repair if necessary. Since we issued AD 2011-24-05, a determination was made that the rototest inspection and applicable corrective actions of a certain fastener hole were inadvertently omitted from the requirements in that AD. This proposed AD would change the inspection compliance times, and, for certain airplanes, would add a one-time ultrasonic inspection for cracking at a certain fastener hole. This proposed AD would also provide optional terminating action for the repetitive inspections. We are proposing this AD to detect and correct cracking of the fastener holes, which could result in rupture of the keel beam, and consequent reduced structural integrity of the airplane.
Qualifications of Drivers; Diabetes Standard
FMCSA proposes to permit drivers with stable, well-controlled insulin-treated diabetes mellitus (ITDM) to be qualified to operate commercial motor vehicles (CMVs) in interstate commerce. Currently, drivers with ITDM are prohibited from driving CMVs in interstate commerce unless they obtain an exemption from FMCSA. This NPRM would enable individuals with ITDM to obtain a Medical Examiner's Certificate (MEC), from a medical examiner (ME) at least annually in order to operate in interstate commerce if the treating clinician (TC) who is the healthcare professional responsible for prescribing insulin for the driver's diabetes, provides documentation to the ME that the condition is stable and well-controlled.
Request for Comments of a Previously Approved Information Collection: Effective U.S. Control (EUSC)/Parent Company
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 is being forwarded to the Office of Management and Budget (OMB) for review and comments. A Federal Register Notice with a 60-day comment period soliciting comments on the following information collection was published on January 21, 2015 (80 FR 3005).
Request for Comments of a Previously Approved Information Collection: Regulations for Making Excess or Surplus Federal Property Available to the U.S. Merchant Marine Academy, State Maritime Academies and Non-Profit Maritime Training Facilities
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 is being forwarded to the Office of Management and Budget (OMB) for review and comments. A Federal Register Notice with a 60-day comment period soliciting comments on the following information collection was published on January 21, 2015 (Federal Register 3006, Vol. 80, No. 13).
Requested Administrative Waiver of the Coastwise Trade Laws: Vessel VANISHING GIRL; Invitation for Public Comments
As authorized by 46 U.S.C. 12121, 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.
Requested Administrative Waiver of the Coastwise Trade Laws: Vessel MOKULANI; Invitation for Public Comments
As authorized by 46 U.S.C. 12121, 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.
Notice of Availability for the Cal Black Memorial Airport Final Supplemental Environmental Impact Statement (Draft SEIS) and Section 4(f) Evaluation
In accordance with the National Environmental Policy Act of 1969 (NEPA, 42 U.S.C. 4321 et seq.) and Council on Environmental Quality regulations (40 CFR part 1500-1508), the Federal Aviation Administration announces the availability of the Final Supplemental Environmental Impact Statement (Final SEIS) and Section 4(f) Evaluation for the Cal Black Memorial Airport. The Section 4(f) Evaluation was prepared pursuant to Section 4(f) of the Department of Transportation Act of 1966 (recodified at 49 U.S.C. 303(c)).
National Express Transit Corporation-Acquisition of Control-Trans Express, Inc., and Rainbow Management Service Inc.
National Express Transit Corporation (NETC or Applicant) has filed an application under 49 U.S.C. 14303 to acquire control of Trans Express Inc. (Trans Express) and Rainbow Management Service Inc. (Rainbow) (together, Acquisition Carriers). The Board is tentatively approving and authorizing the transaction and, if no opposing comments are timely filed, this notice will be the final Board action. Persons wishing to oppose the application must follow the rules at 49 CFR 1182.5 and 1182.8.
Parts and Accessories Necessary for Safe Operation; Application for an Exemption From the Entertainer Motorcoach Council
FMCSA requests public comment on an application for exemption from the Entertainer Motorcoach Council (EMC) to allow its members to operate certain vehicles that do not meet the emergency exit requirements in the Federal Motor Carrier Safety Regulations (FMCSRs). The FMCSRs require buses with a gross vehicle weight rating (GVWR) of more than 10,000 pounds, manufactured on or after September 1, 1994, to meet the emergency exit requirements of Federal Motor Vehicle Safety Standard (FMVSS) No. 217, ``Bus Emergency exits and window retention and release'' in effect on the date of manufacture. FMVSS No. 217 requires side exits and at least one rear exit, but when the bus configuration precludes installation of an accessible rear exit, a roof exit is required in the rear half of the bus to provide a means of egress when the bus is overturned on either side. EMC believes that while certain ``Entertainer Coaches'' do not have a rear or roof exit, the emergency exit windows at the rear sides of the vehicle that open manually and provide openings large enough to admit unobstructed passage provide an equivalent level of safety.
Hours of Service of Drivers: Application for Exemption; American Trucking Associations, Inc.
FMCSA announces that the American Trucking Associations, Inc. (ATA) has applied for an exemption from the Federal hours-of-service (HOS) regulations that prohibit commercial motor vehicle (CMV) drivers from driving a CMV if more than 8 consecutive hours have passed since the driver's last off-duty or sleeper-berth period of 30 minutes or more. ATA is requesting the exemption on behalf of all motor carriers that transport hazardous materials (HM) shipments requiring security plans under regulations of the Pipeline and Hazardous Materials Safety Administration (PHMSA). These plans normally require a driver to ``attend'' such cargo while the CMV is stopped, which would be an on- duty activity. This forces drivers to choose between FMCSA's off-duty rest break requirement and compliance with PHMSA's security plans, many of include an on-duty ``attendance'' requirement. ATA proposes that drivers transporting HM for motor carriers required to file security plans be allowed to count their on-duty ``attendance'' time for any HM cargo toward the required 30-minute rest break requirement, provided the drivers perform no other on-duty activity. The exemption would thus resemble Section 397.7, which requires drivers transporting certain explosives constantly to ``attend'' their load, while Section 395.1(q) allows them to count ``attendance'' time toward their rest break. FMCSA requests public comments on the request for exemption.
Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines
We are revising airworthiness directive (AD) 2014-17-08 for all Pratt & Whitney Canada Corp. (P&WC) PT6A-114 and PT6A-114A turboprop engines. AD 2014-17-08 required initial and repetitive borescope inspections (BSIs) of compressor turbine (CT) blades, and the removal from service of blades that fail inspection. This new AD adds an additional single crystal CT blade, reduces the affected population, and corrects the Credit for Previous Action paragraph. This AD was prompted by P&WC development of an additional single crystal CT blade that corrects the unsafe condition. We are issuing this AD to prevent failure of CT blades, which could result in damage to the engine and damage to the airplane.
Airworthiness Directives; Pilatus Aircraft LTD. Airplanes
We propose to adopt a new airworthiness directive (AD) for Pilatus Aircraft Ltd. Model PC-12/47 and PC-12/47E airplanes. 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 the aileron trim tab disconnecting above 10,000 feet altitude. We are issuing this proposed AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747- 200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes. This proposed AD was prompted by several reports of chafing of the wire bundles inside the electrical conduit of the forward and aft boost pumps of the numbers 1 and 4 main fuel tanks due to high vibration. These wire bundles can chafe through the wire sleeving into the insulation, exposing the wire conductors. This proposed AD would require replacing the wire bundles inside the electrical conduit of the forward and aft boost pumps of the numbers 1 and 4 main fuel tanks with new, improved wire bundles inserted into conduit liners. We are proposing this AD to prevent chafing of the wire bundles and subsequent arcing between the wiring and the electrical conduit creating an ignition source in the fuel tanks, which could result in a fire and consequent fuel tank explosion.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 787 airplanes. This AD requires a repetitive maintenance task for electrical power deactivation on Model 787 airplanes. This AD was prompted by the determination that a Model 787 airplane that has been powered continuously for 248 days can lose all alternating current (AC) electrical power due to the generator control units (GCUs) simultaneously going into failsafe mode. This condition is caused by a software counter internal to the GCUs that will overflow after 248 days of continuous power. We are issuing this AD to prevent loss of all AC electrical power, which could result in loss of control of the airplane.
Proposed Establishment of Class E Airspace and Modification of Class D Airspace; Ogden, Hill AFB, UT
This action proposes to establish Class E airspace and modify Class D airspace at Hill Air Force Base (AFB), Ogden, UT. This action, initiated by the FAA's biennial review of the airspace area, would enhance the safety and management of Instrument Flight Rules (IFR) operations for Standard Instrument Approach Procedures (SIAPs) at the airport. This action would also update the geographic coordinates for Hill AFB, and Ogden-Hinckley Airport.
Proposed Amendment of Class D and Class E Airspace, Revocation of Class E Airspace; Salem, OR
This action proposes to modify Class D airspace, Class E surface area airspace, Class E airspace extending upward from 700 feet above the surface, and remove Class E surface area airspace designated as an extension at McNary Field, Salem, OR. After a biennial review, the FAA found it necessary to amend the airspace area for the safety and management of Instrument Flight Rules (IFR) operations for Standard Instrument Approach Procedures (SIAPs) at the airport.
Proposed Establishment of Class E Airspace, and Amendment of Class D and E Airspace; Ogden-Hinckley Airport, UT
This action proposes to establish Class E airspace as an extension to the Class D surface area, modify Class D airspace, and Class E airspace extending from 700 feet above the surface at Ogden- Hinckley Airport, Ogden, UT. This action, initiated by the FAA's biennial review of the airspace area, would enhance the safety and management of Instrument Flight Rules (IFR) operations for Standard Instrument Approach Procedures (SIAPs) at the airport. This action would also update the geographic coordinates of Ogden-Hinckley Airport and Hill AFB, Ogden, UT.
Airworthiness Directives; General Electric Company CT58 Turboshaft Engines
We propose to supersede airworthiness directives (ADs) 2001- 18-06 and 2008-22-16, which apply to certain General Electric Company (GE) CT58 turboshaft engines. ADs 2001-18-06 and 2008-22-16 require recalculating the lives of life-limited rotating parts using a Repetitive Heavy-Lift (RHL) multiplying factor and removal from service of parts that exceed the recalculated cyclic or hourly life limit. This proposed AD would consolidate ADs 2001-18-06 and 2008-22-16, and further reduce the life capability of certain parts. We are proposing this AD to prevent failure of life-limited rotating parts, uncontained part release, damage to the engine, and damage to the aircraft.
Airworthiness Directives; CFM International S.A. Turbofan Engines
We propose to adopt a new airworthiness directive (AD) for certain CFM International S.A. (CFM) CFM56-7B series turbofan engines. This proposed AD was prompted by reports of uncommanded in-flight shutdowns (IFSDs) on CFM CFM56-7B engines following rupture of the 73- tooth gearshaft located in the engine accessory gearbox (AGB). This proposed AD would require magnetic chip detector (MCD) inspection of the affected gearshafts until removal. We are proposing this AD to prevent failure of certain engine AGB gearshafts, which could lead to failure of one or more engines, loss of thrust control, and damage to the airplane.
Proposed Amendment of Class E Airspace; Jupiter, FL
This action amends Class D Airspace at Jupiter, FL, by removing reference to Restricted Area R-2936 in the regulatory text of the Class D airspace area as the restricted area is no longer needed. This action also updates the geographic coordinates of the airport.
Applications of Eastern Air Lines Group, Inc. for Certificate Authority
The Department of Transportation is directing all interested persons to show cause why it should not issue orders finding Eastern Air Lines Group, Inc. fit, willing, and able, and awarding it certificates of public convenience and necessity authorizing it to engage in interstate and foreign charter air transportation of persons, property, and mail.
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