Department of Transportation June 17, 2016 – Federal Register Recent Federal Regulation Documents

This notice provides information regarding FHWA's finding that a Buy America waiver is appropriate for the use of non-domestic Voith 21/R5 propulsion units compatible with domestic Caterpillar engine 3512C/1600 rpm in the State of Virginia.

The FHWA, on behalf of Caltrans, is issuing this notice to announce actions taken by Caltrans, and USFWS, that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a proposed highway project on Interstate 15 from Cajalco Road, Post Mile (PM) 36.8 to State Route 60 (SR-60) PM 51.4 through the cities of Corona, Norco, Eastvale, and Jurupa Valley, and portions of incorporated Riverside County, State of California. Those actions grant licenses, permits, and approvals for the project.

The U.S. Department of Transportation, Maritime Administration (MARAD) is issuing this notice to cancel the June 14, 2016 U.S. Merchant Marine Academy (``Academy'') Board of Visitors (BOV) meeting scheduled to be held at 2:00 p.m. at the Capital Visitors Center, in Washington, DC. The original Federal Register notice announcing the meeting was published Wednesday, June 1, 2016, 81 FR 35118.

We are revising an earlier proposed airworthiness directive (AD) for certain Dassault Aviation Model MYSTERE-FALCON 50, MYSTERE- FALCON 900, FALCON 900EX, FALCON 2000, and FALCON 2000EX airplanes. The NPRM proposed to require modification of the anti-collision light bonding. The NPRM was prompted by a report of an in-flight lightning strike to the WHELEN anti-collision light located on the top of the vertical fin tip that caused severe damage and resulted in the loss of some airplane functions. This action revises the NPRM by clarifying the applicability. We are proposing this supplemental NPRM (SNPRM) to prevent loss of electrical power and essential airplane functions, and possible reduced control of the airplane. Since these actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.

FMCSA amends its Hazardous Materials Safety Permits rules to update the current incorporation by reference of the Commercial Vehicle Safety Alliance's (CVSA) ``North American Standard Out-of-Service Criteria and Level VI Inspection Procedures and Out-of-Service Criteria for Commercial Highway Vehicles Transporting Transuranics and Highway Route Controlled Quantities of Radioactive Materials as defined in 49 CFR part 173.403.'' Currently the rules reference the April 1, 2015, edition of the out-of-service criteria and, through this final rule, FMCSA incorporates the April 1, 2016, edition.

We propose to supersede airworthiness directive (AD) 2016-04- 12 that applies to certain Turbomeca S.A. Arriel 2B, 2B1, 2C, 2C1, 2C2, 2D, 2E, 2S1, and 2S2 turboshaft engines. AD 2016-04-12 requires spectrometric oil analysis (SOA) inspection of the engine accessory gearbox (AGB), and, depending on the results, removal of the engine AGB. Since we issued AD 2016-04-12, we determined that wear inspections of the engine AGB cover are also required. This proposed AD would require initial and repetitive inspections of the AGB, and wear inspections of the engine AGB cover. We are proposing this AD to prevent failure of the engine AGB, uncommanded in-flight shutdown (IFSD), damage to the engine, and damage to the helicopter.

This rule establishes, amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures (ODPs) 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, adding new obstacles, or changing 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.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures 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, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures 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, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

This action modifies the Class E airspace designated as an extension to the Class D surface area at Ogden-Hinckley Airport, Ogden, UT. The FAA's Aeronautical Information Services identified that the width of the Class E extension to the Class D surface area did not meet the current criteria. This action redefines the controlled airspace area and enhances the safety and management of Standard Instrument Approach Procedures for Instrument Flight Rules (IFR) operations at the airport.

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 777-200 and -300 series airplanes equipped with Rolls-Royce Model RB211-Trent 800 engines. This AD was prompted by reports of thrust reverser (T/R) events related to thermal damage of the T/R inner wall. Depending on the airplane configuration, this AD requires a records review and applicable repetitive inspections, replacements, and installations of the T/R inner wall; and related investigative and corrective actions if necessary. This AD also requires installation of serviceable T/R halves, which would terminate the repetitive actions. This AD also requires revising the inspection or maintenance program by incorporating new airworthiness limitations. We are issuing this AD to detect and correct a degraded T/R inner wall panel. A degraded T/R inner wall panel could lead to failure of the T/R and adjacent components and their consequent separation from the airplane, which could result in a rejected takeoff (RTO) and cause asymmetric thrust and consequent loss of control of the airplane during reverse thrust operation. If a T/R inner wall overheats, separated components could cause structural damage to the airplane, damage to other airplanes, or possible injury to people on the ground.