April 29, 2010 – Federal Register Recent Federal Regulation Documents

Review of Arbitration Awards; Miscellaneous and General Requirements
Document Number: 2010-9996
Type: Proposed Rule
Date: 2010-04-29
Agency: Federal Labor Relations Authority, Agencies and Commissions
The Chairman and Members of the Federal Labor Relations Authority (the Authority) seek public comment on proposed revisions to its regulations concerning review of arbitration awards and the Authority's miscellaneous and general requirements to the extent that they set forth procedural rules that apply to the review of arbitration awards. The purpose of the proposed revisions is to improve and expedite review of such awards.
Requirements for Control Technology Determinations for Major Sources in Accordance With Clean Air Act Sections, Sections 112(g) and 112(j)
Document Number: 2010-9988
Type: Proposed Rule
Date: 2010-04-29
Agency: Environmental Protection Agency
On March 30, 2010, the EPA published a proposed rule to amend the rule governing case-by-case emission limits for major sources of hazardous air pollutants under section 112(j) of the Clean Air Act. We are announcing an extension of the public comment period to May 27, 2010.
Ocean Dumping; Designation of Ocean Dredged Material Disposal Sites Offshore of the Siuslaw River, Oregon
Document Number: 2010-9982
Type: Rule
Date: 2010-04-29
Agency: Environmental Protection Agency
This action finalizes the designation of the Siuslaw River ocean dredged material disposal sites pursuant to the Marine Protection, Research and Sanctuaries Act, as amended (MPRSA). The new sites are needed primarily to serve the long-term need for a location to dispose of material dredged from the Siuslaw River navigation channel, and to provide a location for the disposal of dredged material for persons who have received a permit for such disposal. The newly designated sites will be subject to ongoing monitoring and management to ensure continued protection of the marine environment.
Federal Motor Vehicle Safety Standards; Cargo Carrying Capacity
Document Number: 2010-9981
Type: Rule
Date: 2010-04-29
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document denies petitions for reconsideration of a final rule published December 4, 2007 which amended the Federal motor vehicle safety standards (FMVSS) Nos. 110 and 120 on tire selection and rims.
Airworthiness Directives; Aircraft Industries a.s. Model L 23 Super Blanik Gliders
Document Number: 2010-9951
Type: Proposed Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. 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:
Implantation or Injectable Dosage Form New Animal Drugs; Butorphanol
Document Number: 2010-9871
Type: Rule
Date: 2010-04-29
Agency: Food and Drug Administration, Department of Health and Human Services
The Food and Drug Administration (FDA) is amending the animal drug regulations to reflect approval of an original abbreviated new animal drug application (ANADA) filed by Modern Veterinary Therapeutics, LLC. The ANADA provides for use of an injectable solution of butorphanol tartrate in cats for the relief of pain.
Safety Zone; Private Fireworks, Wilson Creek, Gloucester, VA
Document Number: 2010-9846
Type: Proposed Rule
Date: 2010-04-29
Agency: Coast Guard, Department of Homeland Security
The Coast Guard proposes establishing a safety zone on Wilson Creek in the vicinity of Gloucester, VA in support of a private fireworks event. This action is intended to restrict vessel traffic movement on Wilson Creek to protect mariners from the hazards associated with fireworks displays.
Airworthiness Directives; Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 Airplanes
Document Number: 2010-9609
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
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; Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 2010-9594
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for the products listed above. This 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; Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701 & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) Airplanes
Document Number: 2010-9522
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; Bombardier, Inc. Model DHC-8-400 Series Airplanes
Document Number: 2010-9520
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This 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; British Aerospace Regional Aircraft Model Jetstream Series 3101 and Jetstream Model 3201 Airplanes
Document Number: 2010-9093
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
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; The Boeing Company Model 747-200B Series Airplanes
Document Number: 2010-9091
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Model 747-200B series airplanes. This AD requires repetitive inspections for cracking of the fuselage skin lap joints at stringer 6 on the left and right sides from station (STA) 340 to STA 400, a one- time general visual inspection to determine if certain fasteners are installed and to determine if service repair manual (SRM) repairs or repair doublers are installed, and corrective actions if necessary. Doing an optional modification of the stringer 6 lap joints terminates the repetitive inspections for the modified area. This AD results from reviews done by Boeing, which show that airplanes that were modified by Boeing to the stretched upper deck (SUD) configuration require inspection for cracking of the stringer 6 lap joint upper-fastener row earlier than previously expected. We are issuing this AD to detect and correct cracking of the stringer 6 lap joints where certain external doublers were not installed, which could result in rapid decompression and loss of structural integrity of the airplane.
Airworthiness Directives; Honeywell International Inc., Primus EPIC and Primus APEX Flight Management Systems, Installed on, but not Limited to, Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes, and Pilatus Aircraft Ltd. Model PC-12/47E Airplanes
Document Number: 2010-9090
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Honeywell International Inc., Primus EPIC and Primus APEX flight management systems (FMS), as installed on the airplanes described above. This AD requires revising the Limitations section of the airplane flight manual to incorporate the procedures necessary to recover from or work around a software anomaly in the FMS. This AD results from discovery of software anomalies which, in certain situations, can cause the FMS to generate misleading navigational guidance to the pilots and to the autopilot system of various airplanes having this same system software. We are issuing this AD to provide the flightcrew with procedures to recover from or work around these software anomalies during flight, which could lead to an airplane departing from its scheduled flight path, and result in possible collision with other aircraft or terrain.
Airworthiness Directives; Eurocopter France (ECF) Model EC120B Helicopters
Document Number: 2010-9007
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2010-05-51, which was sent previously to all known U.S. owners and operators of ECF Model EC120B helicopters by individual letters. This AD requires, at specified intervals, inspecting the main rotor head rotor hub (rotor hub) for a crack. If you find scoring, paint flaking or left-over identification plate adhesive, the AD requires sanding the area until the primer coat becomes visible and inspecting the rotor hub for a crack. If you find a crack, the AD requires, before further flight, replacing the rotor hub with an airworthy rotor hub. This amendment is prompted by a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI AD states that ECF has been informed of an emergency landing due to excessive vibrations originating from the main rotor. After an investigation, it was determined that the main rotor head rotor hub (rotor hub) had failed in the attachment area of one of the three drag damper fittings. The actions specified by the AD are intended to prevent failure of a hub, excessive vibrations, loss of a main rotor blade, and subsequent loss of control of the helicopter.
Airworthiness Directives; Eurocopter France Model AS350B, BA, B1, B2, B3, C, D, and D1; AS 355E, F, F1, F2, N, and NP Helicopters
Document Number: 2010-9006
Type: Rule
Date: 2010-04-29
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI AD was issued following the discovery of a potential risk of an untimely squib firing that would cut the hoist cable. A short circuit in the hoist motor brush power supply wiring resulting in an uncommanded squib firing, which cuts the hoist cable, constitutes an unsafe condition.
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