Department of Transportation August 2014 – Federal Register Recent Federal Regulation Documents

This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.

Under the provisions of Title 49, U.S.C. 47153(c), notice is being given that the FAA is considering a request from the Savannah Airport Commission to waive the requirement that a 0.18-acre parcel of surplus property, owned and operated by the Savannah Airport Commission and located adjacent to Georgia Department of Transportation property, be used for aeronautical purposes.

In accordance with the Paperwork Reduction Act of 1995, FMCSA announces its plan to submit the Information Collection Request (ICR) described below to the Office of Management and Budget (OMB) for its review and approval and invites public comment. The primary mission of the Federal Motor Carrier Safety Administration (FMCSA) is to reduce crashes, injuries, and fatalities involving large trucks and buses. Toward that end, FMCSA initiated The Impact of Driver Compensation on Commercial Motor Vehicle Safety Survey. The primary purpose of the study will be to analyze the possible unintended safety consequences of the various methods by which Commercial Motor Vehicle (CMV) drivers in the sample are compensated. Should the study show that there is a relationship between the methods drivers are paid and the methods' effect on safe driving performance, a potential benefit of the study will be to provide CMV carrier companies with information that will help them make more informed decisions about safe operations. In addition to the primary purpose of the study, a number of other potentially potential confounding variables will be assessed. These variables include the following:

FMCSA announces its decision to grant Daimler Trucks North America's (Daimler) application for an exemption for a Daimler driver to drive commercial motor vehicles (CMV) in the United States without possessing a commercial driver's license (CDL) issued by one of the States. The driver is Dr. Wolfgang Bernhard, head of the Daimler Trucks and Bus Division, who will test-drive Daimler vehicles on U.S. roads to better understand product requirements for these vehicles in ``real world'' environments and verify results. He holds a valid German CDL but lacks the U.S. residency necessary to obtain a CDL issued by one of the States. FMCSA believes that the process for obtaining a German- issued CDL is comparable to or is effective as the U.S. CDL requirements and ensures that this driver will likely achieve a level of safety that is equivalent to or greater than the level of safety that would be obtained in the absence of the exemption.

This notice contains a summary of a 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 the petition or its final disposition.

This notice contains a summary of a 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 the petition or its final disposition.

FMCSA requests public comment on an application for exemption from Atwood Forest Products, Inc. (Atwood) to allow the use of a camera system installed at the sides and rear of up to 15 of its commercial motor vehicles (CMV) in lieu of rear-vision mirrors as specified in the Federal Motor Carrier Safety Regulations (FMCSR). Section 393.80 of the FMCSRs currently requires every bus, truck, and truck tractor to be equipped with two rear-vision mirrors, one at each side, firmly attached to the outside of the motor vehicle, and so located as to reflect to the driver a view of the highway to the rear along both sides of the vehicle. All such mirrors must, at a minimum, meet the requirements of Federal Motor Vehicle Safety Standard (FMVSS) No. 111 in effect at the time the vehicle was manufactured. The exemption would enable Atwood to install the camera system on its vehicles for use in an evaluation study, in a location that will offer the best opportunity to optimize data to evaluate the safety and economic benefits of eliminating outside mirrors.

We are adopting a new airworthiness directive (AD) for certain Technify Motors GmbH (type certificate previously held by Thielert Aircraft Engines GmbH) TAE 125-02-99 and TAE 125-02-114 reciprocating engines. This AD requires removal of each high-pressure (HP) fuel pump before 300 flight hours (FHs) in service or within 55 FHs after the effective date of the AD, whichever occurs later. This AD was prompted by in-flight shutdowns on airplanes with TAE 125-02 engines. We are issuing this AD to prevent failure of the HP fuel pump, which could result in damage to the engine and damage to the airplane.

We are adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model BAe 146 series airplanes and Model Avro 146-RJ series airplanes. This AD was prompted by reports of cracking of the main fitting of the nose landing gear (NLG). This AD requires revising the maintenance program by incorporating a new safe- life limitation for the NLG main fitting. We are issuing this AD to prevent collapse of the NLG, which could lead to degradation of direction control on the ground or an un-commanded turn to the left, and a consequent loss of control of the airplane on the ground, possibly resulting in damage to the airplane and injury to occupants.

FMCSA confirms its decision to exempt 72 individuals from its rule prohibiting persons with insulin-treated diabetes mellitus (ITDM) from operating commercial motor vehicles (CMVs) in interstate commerce. The exemptions allow these individuals to operate CMVs in interstate commerce.

We are adopting a new airworthiness directive (AD) for Viking Air Limited Model DHC-3 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as looseness of the horizontal stabilizer actuator mounting block in the forward-aft and side-to-side directions. We are issuing this AD to require actions to address the unsafe condition on these products.

We are adopting a new airworthiness directive (AD) for certain Empresa Brasileira de Aeronautica S.A. (Embraer) Model EMB-135BJ airplanes. This AD was prompted by reports of failure of the bolts that connect the cockpit windshield center-post to the forward fuselage. This AD requires repetitive detailed inspections to detect discrepancies on the attaching parts of the cockpit windshield center- post; checking whether the bolts are tightened, if applicable; and modifying parts, including inspecting for and repairing damage. We are issuing this AD to prevent failed bolts and failed attaching parts of the cockpit windshield center-post, which could lead to loss of structural integrity of the airplane.

We are adopting a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 900EX airplanes. This AD was prompted by our determination of the need for a revision to the airplane airworthiness limitations to introduce a corrosion prevention control program, among other changes, to the maintenance requirements and airworthiness limitations. This AD requires revising the maintenance or inspection program, as applicable, to include the maintenance tasks and airworthiness limitations specified in the Airworthiness Limitations section of the airplane maintenance manual. We are issuing this AD to prevent reduced structural integrity of the airplane, and prevent reduced controllability of the airplane.

The Department of Transportation and the Maritime Administration (MARAD) announces that the Marine Transportation System National Advisory Council (MTSNAC) will meet on September 11, 2014. In January 2014, MARAD held a three-day National Maritime Strategy Symposium to discuss issues facing U.S.-flag vessels. The purpose of this initial public meeting was to generate ideas to improve, strengthen, and sustain the cargo opportunities and sealift capacity of the U.S.-flagged fleet engaged in international commercial trade. A second symposium was held in May which focused on domestic shipping, shipbuilding, ports and the needs of maritime stakeholders on the inland waterways, Great Lakes, gulf and coastwise trade. This meeting will be closed pursuant to 5 U.S.C. 552b(c)(3) in order to deliberate on pre-decisional Agency policy documents containing selected concepts submitted to MARAD from interested members of the public during the two symposiums and as comments in response to meeting notices published in the Federal Register to facilitate the development of a National Maritime Strategy (NMS). The input MARAD receives from the Council will be part of its on-going deliberations as it prepares a long term maritime strategy. As this national maritime strategy develops, MARAD will continue to provide additional opportunities for the public to comment.

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.

We propose to supersede Airworthiness Directive (AD) 2014-09- 05, for certain Airbus Model A330-200 and -300 series airplanes, and Model A340-200 and -300 series airplanes. AD 2014-09-05 currently requires repetitive inspections of certain sidestay upper cardan pins of the main landing gear (MLG), and associated nuts and retainer assemblies, and pin replacement if necessary. Since we issued AD 2014- 09-05, we have determined that a previously optional measurement is necessary to address the identified unsafe condition. We are proposing this AD to detect and correct migration of the sidestay upper cardan pin, which could result in disconnection of the sidestay upper arm from the airplane structure, and could result in a landing gear collapse and consequent damage to the airplane and injury to occupants.

We propose to adopt a new airworthiness directive (AD) for all Empresa Brasileira de Aeronautica S.A. (Embraer) Model EMB-135BJ airplanes. This proposed AD was prompted by a determination that more restrictive fuel limitations are needed. This proposed AD would require revising the maintenance or inspection program to incorporate new compliance times and fuel limitations. We are proposing this AD to detect and correct fatigue cracking of various structural elements and prevent ignition sources in the fuel system.

This document corrects a date and citation in a Federal Register notice published on Friday, July 25, 2014 (79 FR 43530) that announced an information collection request (OMB Control No. 201106- 2127-007) was forwarded to the Office of Management and Budget for review and comment.

We propose to supersede Airworthiness Directive (AD) 2011-09- 11, which applies to certain The Boeing Company Model 777-200 and -300 series airplanes. AD 2011-09-11 currently requires repetitive inspections for hydraulic fluid contamination of the interior of the strut disconnect assembly; repetitive inspections for discrepancies of the interior of the strut disconnect assembly, if necessary; repetitive inspections of the exterior of the strut disconnect assembly for cracks, if necessary; corrective action if necessary; and an optional terminating action for the inspections. Since we issued AD 2011-09-11, we have received reports of side and top cover plates installed with missing fastener bolts, which results in an unsealed opening on the system disconnect assembly. This proposed AD would add, for certain airplanes, an inspection of the side and top cover plates to determine if all cover plate attach fasteners have been installed, and installing any missing fasteners including doing an inspection for damage, and repair if necessary. We are proposing this AD to detect and correct hydraulic fluid contamination, which can cause cracking of titanium parts in the system disconnect assembly; and also to detect and correct missing fasteners, which results in unsealed openings on the system disconnect assembly. Both unsafe conditions can compromise the engine firewall and result in fire hazards for both the engine compartment and the strut.

We propose to supersede Airworthiness Directive (AD) 98-22-10, which applies to certain The Boeing Company Model 737-100, -200, -200C, and -300 series airplanes. AD 98-22-10 currently requires repetitive inspections for cracking of the aft frame and frame support structure of the forward service doorway, and repair if necessary. AD 98-22-10 also provides for an optional terminating action for the repetitive inspection requirements of that AD. Since we issued AD 98-22-10, we have determined that additional inspections are needed, and that additional airplanes may be subject to the identified unsafe condition. This proposed AD would add inspections and add airplanes to the applicability. For certain airplanes, this proposed AD provides a preventive modification, which would terminate the repetitive inspections. We are proposing this AD to detect and correct fatigue cracking of the aft frame and frame support structure of the forward service doorway around the six doorstop fittings, which could result in door deflection and loss of pressurization.

In accordance with the requirements of 49 U.S.C. 5117(c), PHMSA is publishing the following list of special permit applications that have been in process for 180 days or more. The reason(s) for delay and the expected completion date for action on each application is provided in association with each identified application.