March 11, 2016 – Federal Register Recent Federal Regulation Documents

Results 151 - 156 of 156
Endangered and Threatened Wildlife and Plants; Removing the Greater Yellowstone Ecosystem Population of Grizzly Bears From the Federal List of Endangered and Threatened Wildlife
Document Number: 2016-05167
Type: Proposed Rule
Date: 2016-03-11
Agency: Fish and Wildlife Service, Department of the Interior
The best available scientific and commercial data indicate that the Greater Yellowstone Ecosystem (GYE) population of grizzly bears (Ursus arctos horribilis) has recovered and no longer meets the definition of an endangered or threatened species under the Endangered Species Act, as amended (Act). The United States Fish and Wildlife Service (Service) is also proposing to identify the GYE grizzly bear population as a distinct population segment (DPS). Therefore, we, the Service propose to revise the List of Endangered and Threatened Wildlife, under the authority of the Act, by removing the GYE population. The Service has determined that the GYE grizzly bear population has increased in size and more than tripled its occupied range since being listed as threatened under the Act in 1975 and that threats to the population are sufficiently minimized. The participating States of Idaho, Montana, and Wyoming must adopt the necessary post- delisting management objectives, which adequately ensure that the GYE population of grizzly bears remains recovered, into enforceable regulations before the Service will proceed with a final delisting rule.
Airworthiness Directives; MD Helicopters, Inc. (MDHI) Helicopters
Document Number: 2016-04982
Type: Rule
Date: 2016-03-11
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain MDHI Model 369A (Army OH-6A), 369H, 369HE, 369HM, 369HS, 369D, 369E, 369F, 369FF, and 500N helicopters. This AD requires inspecting the auxiliary fuel pump (fuel pump) wire routing in the left-hand fuel cell and corrective action, if necessary. This AD also requires installing a warning decal on the left-hand fuel cell access cover. This AD was prompted by accidents resulting from incorrectly positioned fuel pump wiring within the fuel tank interfering with the operation of the fuel quantity sensor float, which caused an erroneous fuel quantity indication in the cockpit. The actions are intended to detect and correct routing of the fuel pump wiring to prevent interference with the fuel quantity sensor float, an erroneous fuel quantity indication in the cockpit, and subsequent fuel exhaustion and emergency landing.
Airworthiness Directives; Airbus Helicopters
Document Number: 2016-04981
Type: Rule
Date: 2016-03-11
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS 365 N3, EC 155B, and EC155B1 helicopters with certain external life rafts. This AD requires installing a sheath kit on the left-hand and right-hand raft deployment control systems. This AD is prompted by a report that the life raft deployment control could not be adjusted due to problems with the life raft deployment linkage. This unsafe condition, if not corrected, could result in failure of the external life raft to deploy and prevent evacuation of passengers during an emergency.
Improving and Expanding Training Opportunities for F-1 Nonimmigrant Students With STEM Degrees and Cap-Gap Relief for All Eligible F-1 Students
Document Number: 2016-04828
Type: Rule
Date: 2016-03-11
Agency: Department of Homeland Security
The Department of Homeland Security (DHS) is amending its F-1 nonimmigrant student visa regulations on optional practical training (OPT) for certain students with degrees in science, technology, engineering, or mathematics (STEM) from U.S. institutions of higher education. Specifically, the final rule allows such F-1 STEM students who have elected to pursue 12 months of OPT in the United States to extend the OPT period by 24 months (STEM OPT extension). This 24-month extension effectively replaces the 17-month STEM OPT extension previously available to certain STEM students. The rule also improves and increases oversight over STEM OPT extensions by, among other things, requiring the implementation of formal training plans by employers, adding wage and other protections for STEM OPT students and U.S. workers, and allowing extensions only to students with degrees from accredited schools. As with the prior 17-month STEM OPT extension, the rule authorizes STEM OPT extensions only for students employed by employers who participate in E-Verify. The rule also includes the ``Cap-Gap'' relief first introduced in a 2008 DHS regulation for any F- 1 student with a timely filed H-1B petition and request for change of status.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-04564
Type: Rule
Date: 2016-03-11
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2013-08-23 for all The Boeing Company Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10- 30F, MD-11, and MD-11F airplanes. AD 2013-08-23 required adding design features to detect electrical faults and to detect a pump running in an empty fuel tank. This new AD would clarify certain requirements and remove a terminating action. This new AD would also provide an optional method of compliance for the proposed actions. This AD was prompted by a determination that it is necessary to clarify the requirements for the design features and to remove a terminating action for certain inspections. We are issuing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Document Number: 2016-04417
Type: Rule
Date: 2016-03-11
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 96-12-12, which applies to certain Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, and PA-31-350 airplanes. AD 96-12-12 requires a one-time inspection of the bulkhead assembly at fuselage station (FS) 317.75 for cracks and the installation of one of two reinforcement kits determined by whether cracks were found during the inspection. This new AD requires repetitive inspections of the bulkhead assembly at FS 317.75 for cracks, repair of cracks as necessary, and the installation of a reinforcement modification. This AD was prompted by cracks found in the FS 317.75 upper bulkhead. We are issuing this AD to correct the unsafe condition on these products.
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.